| Profil |
Commentaire |
Epaisseur |
| A18 (ORIGINAL) |
|
8.71 |
| A18 (SMOOTHED) |
|
0.00 |
| ABRIAL 17 |
|
12.00 |
| ABRIAL 18 |
|
7.28 |
| ABRIAL STAÉ 230 F3 MOD |
|
|
| ABRIAL STAÉ 230 F4 MOD |
|
|
| ABRIAL STAÉ 230 F5 MOD |
|
|
| ABRIAL STAÉ 230 F6 MOD |
|
|
| ABRIAL STAÉ 230 F2 |
|
|
| AEROSPATIALE RA 1 6 3C3 |
|
|
| AEROSPATIALE RA 1 6 3CW3 |
|
|
| AH 79-100 A |
|
0.00 |
| AH 79-100 B |
|
0.00 |
| AH 79-100 C |
|
0.00 |
| AH-6-40-7 |
|
0.00 |
| AH-6-407 |
|
6.85 |
| AH-7-47-6 |
|
0.00 |
| AH21 |
|
0.00 |
| AH79100A |
|
10.00 |
| ANTARES |
Pour planeur vol de plaine - vol de pente - course aux pylônes - F3B |
10.80 |
| AQUILA |
|
9.38 |
| AQUILA 9.3% SMOOTHED |
|
9.30 |
| AR193S75 |
|
10.20 |
| ARA-D 10% |
|
10.00 |
| ARA-D 13% |
|
13.00 |
| ARA-D 20% |
|
20.00 |
| ARA-D 6% |
|
6.00 |
| AUTOSTABLE 10 |
|
10.00 |
| AUTOSTABLE 12 |
|
12.00 |
| B 29 EMPLANTURE |
|
22.00 |
| B 29 SAUMON |
|
9.00 |
| B-10355B |
|
9.94 |
| B-29 ROOT |
|
0.00 |
| B-8356-B |
|
8.10 |
| B-8406-C |
|
8.00 |
| BAR-2195 |
|
9.49 |
| BE 50 |
|
7.31 |
| BE50 (ORIGINAL) |
|
0.00 |
| BELL 540 |
MODIFIED NACA 0012 |
0.00 |
| BELL/WORTMANN FX 69-H-083 |
|
0.00 |
| BELL/WORTMANN FX 69-H-098 |
|
0.00 |
| BENEDEK 10305-B |
|
|
| BENEDEK 10355 |
|
|
| BERTIN E 55-166 |
|
|
| BERTIN E1 55-166 V |
|
|
| BERTIN E1 55-180 V |
|
|
| BOBWHITE |
|
6.29 |
| BOEING |
|
0.00 |
| BOEING 103 |
|
0.00 |
| BOEING 106 |
|
0.00 |
| BOEING 707 .08 SPAN |
|
0.00 |
| BOEING 707 .19 SPAN |
|
0.00 |
| BOEING 707 .40 SPAN |
|
0.00 |
| BOEING 707 .54 SPAN |
|
0.00 |
| BOEING 707 .99 SPAN |
|
0.00 |
| BOEING 737 MIDSPAN |
|
0.00 |
| BOEING 737 MIDSPAN_1 |
|
0.00 |
| BOEING 737 OUTBOARD |
|
0.00 |
| BOEING 737 ROOT |
|
0.00 |
| BOEING BACXXX |
|
0.00 |
| BOEING VERTOL V(1.95)3009-1.25 |
|
0.00 |
| BOEING VERTOL V13006-.7 |
|
0.00 |
| BOEING VERTOL V43012-1.58 |
|
0.00 |
| BOEING VERTOL V43015-2.48 |
|
0.00 |
| BOEING-VERTOL V23010-1.58 |
|
0.00 |
| BOEING-VERTOL VR-1 |
|
0.00 |
| BOEING-VERTOL VR-11X |
|
0.00 |
| BOEING-VERTOL VR-12 |
|
0.00 |
| BOEING-VERTOL VR-13 |
|
0.00 |
| BOEING-VERTOL VR-14 |
|
0.00 |
| BOEING-VERTOL VR-15 |
|
0.00 |
| BOEING-VERTOL VR-5 |
|
0.00 |
| BOEING-VERTOL VR-7 |
|
0.00 |
| BOEING-VERTOL VR-8 |
|
0.00 |
| BOEING-VERTOL VR-9 |
|
0.00 |
| BOING103 |
|
12.76 |
| C-62 |
|
7.95 |
| CAP 21 |
|
|
| CAST 10-2/DOA 2 |
|
0.00 |
| CH10 (SMOOTHED) |
|
0.00 |
| CHEN |
|
0.00 |
| CJ-3309 |
|
9.48 |
| CJ-5 |
|
9.29 |
| CLARK CYH |
|
|
| CLARK K |
|
0.00 |
| CLARK V |
|
0.00 |
| CLARK W |
|
0.00 |
| CLARK X |
|
11.70 |
| CLARK Y |
Profil Plat |
11.70 |
| CLARK YH |
|
11.70 |
| CLARK YM-15 |
|
0.00 |
| CLARK YM-18 |
|
0.00 |
| CLARK YS |
|
11.70 |
| CLARK Z |
|
0.00 |
| CLARK-CY |
|
11.70 |
| CLARK-V |
|
11.68 |
| CLARK-W |
|
11.22 |
| CLARK-X |
|
11.70 |
| CLARK-Y |
|
11.69 |
| CLARK-YH |
|
11.90 |
| CLARK-YS |
|
11.70 |
| CLARK-Z |
|
11.75 |
| CLARKY |
|
11.70 |
| CLARKY1 |
|
11.70 |
| CLARKY2 |
|
11.69 |
| CLARKYPT |
|
11.72 |
| CR001SM |
|
0.00 |
| CURTISS CR-1 |
|
0.00 |
| DAE 21 |
|
11.78 |
| DAE 51 |
|
9.38 |
| DAE-11 |
|
12.82 |
| DAE-31 |
|
11.06 |
| DAE-51 |
|
9.33 |
| DAVIS |
|
0.00 |
| DAVIS BASIC B-24 WING |
|
0.00 |
| DAVISSM |
|
0.00 |
| DEFIANT CANARD BL110 |
|
0.00 |
| DEFIANT CANARD BL145 |
|
0.00 |
| DEFIANT CANARD BL20 |
|
0.00 |
| DF 101 |
|
0.00 |
| DF-101 |
|
10.97 |
| DF102 |
|
0.00 |
| DFVLR R-4 |
|
0.00 |
| DH4009SM |
|
0.00 |
| DORNIER A-5 |
|
0.00 |
| DOUGLAS LA203A |
|
0.00 |
| DSMA-523A |
|
0.00 |
| DSMA-523B |
|
0.00 |
| DU86-084/18 8.44% |
|
0.00 |
| DU868418 |
|
8.44 |
| DUNH |
|
9.65 |
| DUNHAM |
|
9.65 |
| E 169 DICKE 12.28% |
|
9.84 |
| E-61 |
|
5.67 |
| E-62 |
|
5.46 |
| E10(08%) |
|
8.00 |
| E168 (12.45%) |
|
12.45 |
| E169 (14.4%) |
|
14.40 |
| E174 (DICKE 8.92%) |
|
8.92 |
| E176 (8.83%) |
|
8.83 |
| E178 (8.69%) |
|
8.69 |
| E180 (8.59%) |
|
8.59 |
| E182 (8.47%) |
|
8.47 |
| E184 (8.33%) |
|
8.33 |
| E186 (10.27%) |
|
10.27 |
| E193 (10.22%) |
|
10.22 |
| E195 (11.82%) |
|
11.82 |
| E197 (13.49%) |
|
13.49 |
| E201 (11.88%) |
|
11.88 |
| E203 (13.64%) |
|
13.64 |
| E205 (10.48%) |
|
10.48 |
| E2052595 |
|
9.50 |
| E207 (12.04%) |
|
12.04 |
| E209 (13.72%) |
|
13.72 |
| E210 (13.64%) |
|
13.64 |
| E211 (10.96%) |
|
10.96 |
| E212 (10.55%) |
|
10.55 |
| E214 (11.1%) |
|
11.10 |
| E216 (10.4%) |
|
10.40 |
| E220 (11.48%) |
|
11.48 |
| E221 (9.39%) |
|
9.39 |
| E222 (10.17%) |
|
10.17 |
| E224 (10.17%) |
|
10.17 |
| E226 (10.19%) |
|
10.19 |
| E230 (9.96%) |
|
9.96 |
| E231 |
|
0.00 |
| E385 (8.41%) |
|
8.41 |
| E392 (10.15%) |
|
10.15 |
| E423 |
|
0.00 |
| E471 (6.25%) |
|
6.25 |
| E474 (14.09%) |
|
14.09 |
| E475 (15.01%) |
|
15.01 |
| E61 (5.64%) |
|
5.64 |
| E62 (5.62%) |
|
5.62 |
| E63 (4.25%) |
|
4.25 |
| E64 (8.45%) |
|
8.45 |
| E71 (5.15%) |
|
5.15 |
| EB-15-10 |
|
10.00 |
| EB-380 |
Profil étudié à partir des EP-374 et EP-387 -perfo = Ep-193 ou Fx 60-126 |
10.00 |
| EH 0.0/9.0 |
|
0.00 |
| EH 1.0/9.0 |
|
0.00 |
| EH 1.5/9 |
|
9.00 |
| EH 1.5/9.0 |
|
0.00 |
| EH 1/7 |
|
7.00 |
| EH 1/9 |
|
9.00 |
| EH 2.0/10 |
|
0.00 |
| EH 2.0/12 |
|
0.00 |
| EH 2.5/10 |
|
0.00 |
| EH 2/10 |
|
10.00 |
| EH 3.0/12 |
|
0.00 |
| EH-0-9 |
|
9.00 |
| EH-10-9 |
|
9.02 |
| EH-15-9 |
|
10.05 |
| EH-16-10 |
|
9.06 |
| EH-20-10 |
|
10.12 |
| EP193120 |
|
10.11 |
| EPP-168 |
Etudé pour les avions de voltige corde mini 240 vol dos T bien |
12.44 |
| EPP-169 |
Etudié pour les avions de voltige corde mini 240 vol dos T bien |
14.40 |
| EPP-174 |
Eppler 174
182 série pour ailes volantes
profils évolutifs ou planeur rapide |
8.90 |
| EPP-176 |
Eppler 174
182 série pour ailes volantes
profils évolutifs |
8.69 |
| EPP-178 |
Eppler 174
182 série pour ailes volantes
profils évolutifs ou planeur rapide |
8.70 |
| EPP-180 |
Eppler 174
182 série pour ailes volantes
profils évolutifs |
8.55 |
| EPP-182 |
Eppler 174
182 série pour ailes volantes
profils évolutifs ou planeur rapide |
8.38 |
| EPP-184 |
Profil autostable pour ailes delta |
8.40 |
| EPP-186 |
Profil pour aile volante corde mini 200 allongement max 10 centrage 15 |
9.15 |
| EPP-193 |
Profil utilisable du 2 axes au F3B centrage max 35 % |
10.20 |
| EPP-193K |
Profil utilisable du 2 axes au F3B centrage max 35 % volet de 24% |
10.22 |
| EPP-195 |
Pour grands planeurs allongement 15
20 corde mini 180 centrage
30% |
11.85 |
| EPP-197 |
Pour grands planeurs allongement 15
20 corde mini 180 centrage
30% |
13.50 |
| EPP-201 |
Pour grands planeurs allongement 15
20 corde mini 180 centrage
30% |
12.00 |
| EPP-203 |
Pour grand planeur de voltige et thermique centrage
30% |
13.50 |
| EPP-205 |
Pour planeurs type F3B ou vol de pente (thermique avec transitions rapides) |
10.50 |
| EPP-205K |
Pour planeurs vol de pente ou thermique ou lectrique |
9.20 |
| EPP-207 |
|
12.04 |
| EPP-209 |
|
13.50 |
| EPP-210 |
Profil trés porteur pour grands planeur ou avion |
13.64 |
| EPP-211 |
|
10.90 |
| EPP-211K |
|
8.00 |
| EPP-212 |
|
10.50 |
| EPP-214 |
Pour F3B
utiliser avec volets
-6ø a grand vitesse (polaire avec volets) |
11.00 |
| EPP-220 |
Pour les racers |
11.50 |
| EPP-221 |
Pour la vitesse avion |
9.40 |
| EPP-222 |
Du Ep-222 au Ep-230 profils pour aile volante - utilisable seul sur planeur |
10.08 |
| EPP-224 |
Du Ep-222 au Ep-230 profils pour aile volante - utilisable seul sur planeur |
10.17 |
| EPP-226 |
Du Ep-222 au Ep-230 profils pour aile volante |
10.20 |
| EPP-228 |
Du Ep-222 au Ep-230 profils pour aile volante |
10.00 |
| EPP-230 |
Du Ep-222 au Ep-230 profils pour aile volante |
9.97 |
| EPP-374 |
pour planeur de pente et voltige mme de F3B et avion |
10.90 |
| EPP-385 |
|
8.20 |
| EPP-385M |
|
10.00 |
| EPP-387 |
|
9.10 |
| EPP-387M |
|
10.10 |
| EPP-392 |
|
10.15 |
| EPP-393 |
Du planeur thermique au grand planeur de pente - centrage 35
38% |
12.00 |
| EPP-471 |
|
6.20 |
| EPP-474 |
Etudié pour les avions de voltige corde mini 240 vol dos T bien |
14.10 |
| EPP-475 |
Etudi pour les avions de voltige corde mini 240 vol dos T bien |
15.00 |
| EPP-67 |
Pour grand planeur pas trop rapide style maquette |
11.62 |
| EPPLER 1098 |
|
0.00 |
| EPPLER 1200 |
|
0.00 |
| EPPLER 1210 |
|
0.00 |
| EPPLER 1211 |
|
0.00 |
| EPPLER 1213 |
|
0.00 |
| EPPLER 1214 |
|
0.00 |
| EPPLER 1230 |
|
0.00 |
| EPPLER 1233 |
|
0.00 |
| EPPLER 168 |
Biconvexe Symétrique Adapté à la voltige avion type;multi. Corde >= 240 m/m.Pas plus de 70 gr/dm°. Calage entre 0° et 0.5°. Centrage 25% |
12.44 |
| EPPLER 169 |
Biconvexe Symétrique Adapté à la voltige avion type;multi. Corde >= 240 m/m.Pas plus de 70 gr/dm°. Calage entre 0° et 0.5°. Centrage 25% |
14.40 |
| EPPLER 174 |
|
8.92 |
| EPPLER 176 |
|
8.83 |
| EPPLER 178 |
Profil de Vitesse. N'aime pas voler lentement.Calage 0° à 0.5°. Centrage 25% à 28% |
8.69 |
| EPPLER 180 |
Profil de Vitesse. N'aime pas voler lentement.Calage 0° à 0.5°. Centrage 25% à 28% |
8.59 |
| EPPLER 182 |
Profil de Vitesse. N'aime pas voler lentement.Calage 0° à 0.5°. Centrage 25% à 28% |
8.47 |
| EPPLER 184 |
Ailes volantes.Transitions rapides et voltige.Ca entre 15 et 25 gr/dm.Centrage 18% |
8.32 |
| EPPLER 186 |
Ailes Volantes. Fortement autostable Ca entre 15 et 25 gr/dm.Centrage 18% |
10.30 |
| EPPLER 193 |
|
10.22 |
| EPPLER 195 |
|
11.82 |
| EPPLER 197 |
|
13.50 |
| EPPLER 201 |
|
11.88 |
| EPPLER 203 |
|
13.57 |
| EPPLER 205 |
Profil Plat |
10.48 |
| EPPLER 207 |
|
11.94 |
| EPPLER 209 |
|
13.70 |
| EPPLER 210 |
|
13.64 |
| EPPLER 211 |
Supporte les petites cordes Modèles vifs et voltigeurs.
|
10.80 |
| EPPLER 212 |
|
10.56 |
| EPPLER 214 |
|
11.10 |
| EPPLER 216 |
|
10.43 |
| EPPLER 220 |
|
11.45 |
| EPPLER 221 |
|
9.33 |
| EPPLER 222 |
|
10.17 |
| EPPLER 224 |
|
10.17 |
| EPPLER 226 |
|
10.17 |
| EPPLER 228 |
|
10.06 |
| EPPLER 230 |
|
9.96 |
| EPPLER 266 |
|
0.00 |
| EPPLER 297 |
|
0.00 |
| EPPLER 325 |
|
0.00 |
| EPPLER 326 |
|
0.00 |
| EPPLER 327 |
|
0.00 |
| EPPLER 328 |
|
0.00 |
| EPPLER 329 |
|
0.00 |
| EPPLER 330 |
|
0.00 |
| EPPLER 331 |
|
0.00 |
| EPPLER 332 |
|
0.00 |
| EPPLER 333 |
|
0.00 |
| EPPLER 334 |
|
0.00 |
| EPPLER 335 |
|
0.00 |
| EPPLER 336 |
|
0.00 |
| EPPLER 337 |
|
0.00 |
| EPPLER 338 |
|
0.00 |
| EPPLER 339 |
|
0.00 |
| EPPLER 340 |
|
0.00 |
| EPPLER 341 |
|
0.00 |
| EPPLER 342 |
|
0.00 |
| EPPLER 343 |
|
0.00 |
| EPPLER 344 |
|
0.00 |
| EPPLER 360 |
|
0.00 |
| EPPLER 361 |
|
0.00 |
| EPPLER 374 |
Biconvexe dissymétriqueA utiliser sur les planeurs de voltige ou de transition 3axes. Calage à 2°, centrage entre 30% et 33% (35% voltige) |
10.92 |
| EPPLER 376 |
|
0.00 |
| EPPLER 377 |
|
0.00 |
| EPPLER 377 (MODIFIED) |
|
0.00 |
| EPPLER 378 |
|
0.00 |
| EPPLER 379 |
|
0.00 |
| EPPLER 385 |
|
8.42 |
| EPPLER 385/MOD 4.0.10.0 |
|
|
| EPPLER 387 |
|
9.00 |
| EPPLER 387 (=E 174) |
|
|
| EPPLER 387/MOD 4.0.10.0 |
|
|
| EPPLER 392 |
|
10.15 |
| EPPLER 393 |
|
0.00 |
| EPPLER 395 |
|
0.00 |
| EPPLER 396 |
|
0.00 |
| EPPLER 397 |
|
0.00 |
| EPPLER 398 |
|
0.00 |
| EPPLER 399 |
|
0.00 |
| EPPLER 403 |
|
0.00 |
| EPPLER 407 |
|
0.00 |
| EPPLER 417 |
|
0.00 |
| EPPLER 420 |
|
0.00 |
| EPPLER 421 |
|
0.00 |
| EPPLER 422 |
|
0.00 |
| EPPLER 426 |
|
0.00 |
| EPPLER 428 |
|
0.00 |
| EPPLER 431 |
|
0.00 |
| EPPLER 432 |
|
0.00 |
| EPPLER 433 |
|
0.00 |
| EPPLER 434 |
|
0.00 |
| EPPLER 435 |
|
0.00 |
| EPPLER 471 |
|
6.25 |
| EPPLER 472 |
|
0.00 |
| EPPLER 473 |
|
0.00 |
| EPPLER 474 |
|
14.00 |
| EPPLER 475 |
|
15.00 |
| EPPLER 476 |
|
0.00 |
| EPPLER 477 |
|
0.00 |
| EPPLER 478 |
|
0.00 |
| EPPLER 479 |
|
0.00 |
| EPPLER 485 |
|
0.00 |
| EPPLER 49 |
|
0.00 |
| EPPLER 502 |
|
0.00 |
| EPPLER 520 |
|
0.00 |
| EPPLER 521 |
|
0.00 |
| EPPLER 540 |
|
0.00 |
| EPPLER 541 |
|
0.00 |
| EPPLER 542 |
|
0.00 |
| EPPLER 543 |
|
0.00 |
| EPPLER 544 |
|
0.00 |
| EPPLER 545 |
|
0.00 |
| EPPLER 546 |
|
0.00 |
| EPPLER 547 |
|
0.00 |
| EPPLER 548 |
|
0.00 |
| EPPLER 549 |
|
0.00 |
| EPPLER 550 |
|
0.00 |
| EPPLER 551 |
|
0.00 |
| EPPLER 552 |
|
0.00 |
| EPPLER 553 |
|
0.00 |
| EPPLER 554 |
|
0.00 |
| EPPLER 555 |
|
0.00 |
| EPPLER 556 |
|
0.00 |
| EPPLER 557 |
|
0.00 |
| EPPLER 558 |
|
0.00 |
| EPPLER 559 |
|
0.00 |
| EPPLER 560 |
|
0.00 |
| EPPLER 561 |
|
0.00 |
| EPPLER 562 |
|
0.00 |
| EPPLER 58 |
|
0.00 |
| EPPLER 580 |
|
0.00 |
| EPPLER 582 |
|
0.00 |
| EPPLER 583 |
|
0.00 |
| EPPLER 584 |
|
0.00 |
| EPPLER 585 |
|
0.00 |
| EPPLER 587 |
|
0.00 |
| EPPLER 59 |
|
|
| EPPLER 593 |
|
0.00 |
| EPPLER 598 |
|
0.00 |
| EPPLER 603 |
|
0.00 |
| EPPLER 604 |
|
0.00 |
| EPPLER 61 |
|
|
| EPPLER 62 |
|
|
| EPPLER 625 |
|
0.00 |
| EPPLER 635 |
|
0.00 |
| EPPLER 636 |
|
0.00 |
| EPPLER 637 |
|
0.00 |
| EPPLER 638 |
|
0.00 |
| EPPLER 639 |
|
0.00 |
| EPPLER 642 |
|
0.00 |
| EPPLER 654 |
|
0.00 |
| EPPLER 655 |
|
0.00 |
| EPPLER 656 |
|
0.00 |
| EPPLER 657 |
|
0.00 |
| EPPLER 66 |
|
10.14 |
| EPPLER 662 |
|
|
| EPPLER 664 |
|
|
| EPPLER 664 (EXTENDED) |
|
0.00 |
| EPPLER 668 |
|
0.00 |
| EPPLER 67 |
|
11.62 |
| EPPLER 678 |
|
0.00 |
| EPPLER 68 |
|
13.10 |
| EPPLER 682 |
|
0.00 |
| EPPLER 694 |
|
0.00 |
| EPPLER 71 |
|
|
| EPPLER 715 |
|
0.00 |
| EPPLER 748 |
|
0.00 |
| EPPLER 793 |
|
0.00 |
| EPPLER 817 HYDROFOIL |
|
0.00 |
| EPPLER 818 HYDROFOIL |
|
0.00 |
| EPPLER 855 |
|
0.00 |
| EPPLER 856 |
|
0.00 |
| EPPLER 857 |
|
0.00 |
| EPPLER 858 |
|
0.00 |
| EPPLER 862 STRUT |
|
0.00 |
| EPPLER 863 STRUT |
|
0.00 |
| EPPLER 864 STRUT |
|
0.00 |
| EPPLER 874 HYDROFOIL |
|
0.00 |
| EPPLER 904 |
|
0.00 |
| EPPLER 908 |
|
0.00 |
| EPPLER E1212 |
|
0.00 |
| EPPLER E1212MOD |
|
0.00 |
| EPPLER E662 |
|
0.00 |
| EPPLER E836 HYDROFOIL |
|
0.00 |
| EPPLER E837 HYDROFOIL |
|
0.00 |
| EPPLER E838 HYDROFOIL |
|
0.00 |
| EPPLER E850 |
|
0.00 |
| EPPLER E851 |
|
0.00 |
| EPPLER E852 |
|
0.00 |
| EPPLER E853 |
|
0.00 |
| EPPLER E854 |
|
0.00 |
| EPPLER EA 6(-1)-009 |
|
0.00 |
| EPPLER EA 6(-1)-012 |
|
0.00 |
| EPPLER EA 8(-1)-006 |
|
0.00 |
| EPPLER EC 86(-3)-914 |
|
0.00 |
| EPPLER STE 87(-3)-914 |
|
0.00 |
| EPPLER STE 871-514 |
|
0.00 |
| EPPLER STF 863-615 |
|
0.00 |
| ESPADA |
|
5.56 |
| FAUVEL |
|
13.98 |
| FUKUDA10 |
|
9.92 |
| FX 38-153 |
|
0.00 |
| FX 60 - 100 |
|
10.00 |
| FX 60 - 126 |
|
12.60 |
| FX 60 - 140 |
|
14.00 |
| FX 60-100 |
|
0.00 |
| FX 60-100 (126) |
|
0.00 |
| FX 60-126/1 |
|
0.00 |
| FX 60-157 |
|
0.00 |
| FX 60-160 |
|
0.00 |
| FX 60-177 |
|
0.00 |
| FX 61-147 |
|
0.00 |
| FX 61-163 |
|
0.00 |
| FX 61-168 |
|
0.00 |
| FX 61-184 |
|
0.00 |
| FX 62 - K131 |
|
13.10 |
| FX 62-K-153/20 |
|
0.00 |
| FX 63 - 120 |
|
12.00 |
| FX 63 - 137 |
|
13.70 |
| FX 63-100 |
|
0.00 |
| FX 63-110 |
|
0.00 |
| FX 63-120 |
|
0.00 |
| FX 63-137 13.7% SMOOTHED |
|
13.70 |
| FX 63-143 |
|
0.00 |
| FX 63-145 |
|
0.00 |
| FX 63-147 |
|
0.00 |
| FX 63-158 |
|
0.00 |
| FX 66-17AII-182 |
|
0.00 |
| FX 66-182 |
|
0.00 |
| FX 66-S-161 |
|
0.00 |
| FX 66-S-171 |
|
0.00 |
| FX 66-S-196 |
|
0.00 |
| FX 66-S-196 V1 |
|
0.00 |
| FX 67-K-150/17 |
|
0.00 |
| FX 67-K-170/17 |
|
0.00 |
| FX 71 - L150/K30 |
|
15.00 |
| FX 71-L-150/20 |
|
0.00 |
| FX 71-L-150/25 |
|
0.00 |
| FX 71-L-150/K30 |
|
0.00 |
| FX 74-CL5-140 MOD (SMOOTHED) |
|
0.00 |
| FX LIII-142 K 25 |
|
0.00 |
| FX S 02-196 |
|
0.00 |
| FX S 02/1-158 |
|
0.00 |
| FX S 03-182 |
|
0.00 |
| FX-L142K |
|
14.20 |
| FX-LV152 |
Pour avion de voltige - utilisable avec 25% de volets |
15.20 |
| FX-M2 |
|
8.40 |
| FX60-100 10.0% SMOOTHED |
|
10.00 |
| FX60100 |
|
38.10 |
| FX60100S |
|
9.95 |
| FX60126 |
Profil bon a tout faire - centrage 30
40% |
12.60 |
| FX601261 |
Fx-60-126 redessin et trs lgrement amlior |
12.60 |
| FX60126S |
|
12.54 |
| FX61140 |
|
14.00 |
| FX61147 |
|
14.70 |
| FX61163 |
|
16.30 |
| FX62K131 |
|
13.10 |
| FX62K153 |
|
15.30 |
| FX63100 |
|
9.92 |
| FX63110 |
|
11.00 |
| FX63137 |
|
13.71 |
| FX6617A2 |
|
18.19 |
| FX66S161 |
|
16.10 |
| FX67K125 |
|
12.50 |
| FX67K150 |
|
14.98 |
| FX71L150 |
Profil pour la voltige avion et planeur |
15.00 |
| FX72150A |
|
15.00 |
| FX72150B |
|
15.00 |
| FX74_CL5_140 |
|
0.00 |
| G-610-B |
|
7.90 |
| GA (W) 1 NASA WHITCOMB |
|
|
| GA (W) 2 NASA WHICOMB |
|
|
| GA-1NASA |
|
17.00 |
| GEMINI (SMOOTHED) |
|
0.00 |
| GIII BL0 |
|
0.00 |
| GIII BL126 |
|
0.00 |
| GIII BL145 |
|
0.00 |
| GIII BL167 |
|
0.00 |
| GIII BL207 |
|
0.00 |
| GIII BL288 |
|
0.00 |
| GIII BL332 |
|
0.00 |
| GIII BL369 |
|
0.00 |
| GIII BL387 |
|
0.00 |
| GIII BL430 |
|
0.00 |
| GIII BL45 |
|
0.00 |
| GIII BL450 |
|
0.00 |
| GIII BL75 |
|
0.00 |
| GIII BL86 |
|
0.00 |
| GM15 (SMOOTHED) |
|
0.00 |
| GOE 100 (SOPWITH) |
|
0.00 |
| GOE 101 |
|
0.00 |
| GOE 10K |
|
0.00 |
| GOE 113 |
|
0.00 |
| GOE 114 (MVA MK.1) |
|
0.00 |
| GOE 115 (MVA MK.2) |
|
0.00 |
| GOE 116 (MVA MK.3) |
|
0.00 |
| GOE 117 (MVA MK.4) |
|
0.00 |
| GOE 118 (MVA MK.7) |
|
0.00 |
| GOE 11K |
|
0.00 |
| GOE 121 (MVA H.1) |
|
0.00 |
| GOE 122 (MVA H.2) |
|
0.00 |
| GOE 123 |
|
0.00 |
| GOE 124 (MVA H.4) |
|
0.00 |
| GOE 12K |
|
0.00 |
| GOE 133 (MVA H.11) |
|
0.00 |
| GOE 134 (MVA H.12) |
|
0.00 |
| GOE 137 (MVA H.15) |
|
0.00 |
| GOE 13K |
|
0.00 |
| GOE 14 |
|
0.00 |
| GOE 140 (MVA H.17) |
|
0.00 |
| GOE 142 (MVA H.19) |
|
0.00 |
| GOE 143 (MVA H.20) |
|
0.00 |
| GOE 144 (MVA H.21) |
|
0.00 |
| GOE 147 (MVA H.6) |
|
0.00 |
| GOE 14K |
|
0.00 |
| GOE 15 |
|
0.00 |
| GOE 155 (SSW D.1) |
|
0.00 |
| GOE 15K |
|
0.00 |
| GOE 164 (MVA MK.10) |
|
0.00 |
| GOE 165 (MVA MK.11) |
|
0.00 |
| GOE 167 (V.KARMAN PROP.2) |
|
0.00 |
| GOE 16K |
|
0.00 |
| GOE 173 (ALBATROS 6020) |
|
0.00 |
| GOE 174 (ALBATROS 5020) |
|
0.00 |
| GOE 176 (ALBATROS 7020) |
|
0.00 |
| GOE 177 |
|
0.00 |
| GOE 178 |
|
0.00 |
| GOE 180 (MVA H.26) |
|
0.00 |
| GOE 182 (MVA H.27) |
|
0.00 |
| GOE 184 (MVA H.29) |
|
0.00 |
| GOE 187 (SCHTTE-LANZ 2U10) |
|
0.00 |
| GOE 188 (SCHTTE-LANZ 3U10) |
|
0.00 |
| GOE 190 (MVA MK.18) |
|
0.00 |
| GOE 195 |
|
0.00 |
| GOE 198 (L.F.G. 5294) |
|
0.00 |
| GOE 199 (L.F.G. 5406) |
|
0.00 |
| GOE 207 (AVIATIK V8) |
|
0.00 |
| GOE 210 (DAIMLER) |
|
0.00 |
| GOE 217 (MVA MK.12) |
|
0.00 |
| GOE 222 (MVA H.33) |
|
0.00 |
| GOE 223 (MVA H.34) |
|
0.00 |
| GOE 225 (MVA H.35) |
|
0.00 |
| GOE 226 (MVA H.36) |
|
0.00 |
| GOE 227 (MVA H.37) |
|
0.00 |
| GOE 228 (MVA H.38) |
|
0.00 |
| GOE 229 (MVA H.39) |
|
0.00 |
| GOE 233 (MVA CA4) |
|
0.00 |
| GOE 234 (MVA CA5) |
|
0.00 |
| GOE 235 (SCHTTE-LANZ) |
|
0.00 |
| GOE 238 (HANSA-BRANDENBURG) |
|
0.00 |
| GOE 239 (MVA H.31) |
|
0.00 |
| GOE 240 (KOLLER) |
|
0.00 |
| GOE 241 (MVA PR.1) |
|
0.00 |
| GOE 242 (MVA PR.2) |
|
0.00 |
| GOE 243 (MVA PR.3) |
|
0.00 |
| GOE 244 (MVA PR.4) |
|
0.00 |
| GOE 255 (MVA CA.6) |
|
0.00 |
| GOE 256 (JUNKERS E) |
|
0.00 |
| GOE 257 |
|
0.00 |
| GOE 264 |
|
0.00 |
| GOE 265 |
|
0.00 |
| GOE 269 |
|
0.00 |
| GOE 274 (DAIMLER V) |
|
0.00 |
| GOE 275 (DAIMLER VI) |
|
0.00 |
| GOE 276 (DAIMLER VII) |
|
0.00 |
| GOE 277 (DAIMLER VIII) |
|
0.00 |
| GOE 278 (DAIMLER IX) |
|
0.00 |
| GOE 279 (DAIMLER X) |
|
0.00 |
| GOE 280 (DAIMLER XI) |
|
0.00 |
| GOE 281 (DAIMLER XII) |
|
0.00 |
| GOE 282 (DAIMLER XIII) |
|
0.00 |
| GOE 284 |
|
0.00 |
| GOE 285 |
|
0.00 |
| GOE 286 |
|
0.00 |
| GOE 287 |
|
0.00 |
| GOE 288 |
|
0.00 |
| GOE 289 (MVA 289) |
|
0.00 |
| GOE 290 (MVA 290) |
|
0.00 |
| GOE 298 |
|
0.00 |
| GOE 29B |
|
0.00 |
| GOE 300 (FRIEDRICHSHAFEN G20) |
|
0.00 |
| GOE 301 (FRIEDRICHSHAFEN G 13) |
|
0.00 |
| GOE 303 (FRIEDRICHSHAFEN G03) |
|
0.00 |
| GOE 304 (FRIEDRICHSHAFEN G02) |
|
0.00 |
| GOE 308 (MVA H.40) |
|
0.00 |
| GOE 309 (MVA H.41) |
|
0.00 |
| GOE 310 (MVA H.42) |
|
0.00 |
| GOE 311 (MVA H.43) |
|
0.00 |
| GOE 314 (HANSA-BRANDENBURG) |
|
0.00 |
| GOE 315 (HANSA-BRANDENBURG III.5) |
|
0.00 |
| GOE 316 (HANSA-BRANDENBURG IV.5) |
|
0.00 |
| GOE 318 (HANSA-BRANDENBURG VI.5) |
|
0.00 |
| GOE 319 (HANSA-BRANDENBURG II) |
|
0.00 |
| GOE 320 (HANSA-BRANDENBURG II.1) |
|
0.00 |
| GOE 321 (HANSA-BRANDENBURG III.1) |
|
0.00 |
| GOE 322 (HANSA-BRANDENBURG IV.1) |
|
0.00 |
| GOE 323 (HANSA-BRANDENBURG V.1) |
|
0.00 |
| GOE 324 (HANSA-BRANDENBURG) |
|
0.00 |
| GOE 325 (PFALZ 54) |
|
0.00 |
| GOE 326 (PFALZ 55) |
|
0.00 |
| GOE 328 |
|
0.00 |
| GOE 329 (PFALZ 58) |
|
0.00 |
| GOE 330 (PFALZ 59) |
|
0.00 |
| GOE 331 (PFALZ 60) |
|
0.00 |
| GOE 332 (PFALZ 61) |
|
0.00 |
| GOE 335 (D.F.W.) |
|
0.00 |
| GOE 336 (MVA H.44) |
|
0.00 |
| GOE 342 |
|
0.00 |
| GOE 344 (PFALZ 71) |
|
0.00 |
| GOE 346 (FRIEDRICHSHAFEN-STAAKEN) |
|
0.00 |
| GOE 358 |
|
0.00 |
| GOE 359 |
|
0.00 |
| GOE 360 |
|
0.00 |
| GOE 361 |
|
0.00 |
| GOE 362 |
|
0.00 |
| GOE 363 |
|
0.00 |
| GOE 364 |
|
0.00 |
| GOE 365 |
|
0.00 |
| GOE 366 |
|
0.00 |
| GOE 367 |
|
0.00 |
| GOE 368 |
|
0.00 |
| GOE 369 |
|
0.00 |
| GOE 370 |
|
0.00 |
| GOE 371 |
|
0.00 |
| GOE 372 |
|
0.00 |
| GOE 373 |
|
0.00 |
| GOE 374 |
|
0.00 |
| GOE 375 |
|
0.00 |
| GOE 376 |
|
0.00 |
| GOE 377 |
|
0.00 |
| GOE 379 |
|
0.00 |
| GOE 380 |
|
0.00 |
| GOE 381 |
|
0.00 |
| GOE 382 |
|
0.00 |
| GOE 383 |
|
0.00 |
| GOE 384 |
|
0.00 |
| GOE 385 |
|
0.00 |
| GOE 386 |
|
0.00 |
| GOE 387 |
|
0.00 |
| GOE 388 |
|
0.00 |
| GOE 389 |
|
0.00 |
| GOE 390 |
|
0.00 |
| GOE 391 |
|
0.00 |
| GOE 392 |
|
0.00 |
| GOE 393 |
|
0.00 |
| GOE 394 |
|
0.00 |
| GOE 395 |
|
0.00 |
| GOE 396 |
|
0.00 |
| GOE 397 |
|
0.00 |
| GOE 398 |
|
0.00 |
| GOE 399 |
|
0.00 |
| GOE 400 |
|
0.00 |
| GOE 401 |
|
0.00 |
| GOE 402 |
|
0.00 |
| GOE 403 |
|
0.00 |
| GOE 404 |
|
0.00 |
| GOE 405 |
|
0.00 |
| GOE 406 |
|
0.00 |
| GOE 407 |
|
0.00 |
| GOE 408 |
|
0.00 |
| GOE 409 |
|
0.00 |
| GOE 410 |
|
0.00 |
| GOE 411 |
|
0.00 |
| GOE 412 |
|
0.00 |
| GOE 413 |
|
0.00 |
| GOE 414 |
|
0.00 |
| GOE 415 |
|
0.00 |
| GOE 416A |
|
0.00 |
| GOE 417 |
|
0.00 |
| GOE 417A (GEW. PLATTE) |
|
0.00 |
| GOE 418 |
|
0.00 |
| GOE 419 |
|
0.00 |
| GOE 420 |
|
0.00 |
| GOE 421 |
|
0.00 |
| GOE 422 |
|
0.00 |
| GOE 423 |
|
0.00 |
| GOE 424 |
|
0.00 |
| GOE 425 |
|
0.00 |
| GOE 426 |
|
0.00 |
| GOE 427 |
|
0.00 |
| GOE 428 |
|
0.00 |
| GOE 429 |
|
0.00 |
| GOE 430 |
|
0.00 |
| GOE 431 |
|
0.00 |
| GOE 432 |
|
0.00 |
| GOE 433 |
|
0.00 |
| GOE 434 |
|
0.00 |
| GOE 435 |
|
0.00 |
| GOE 436 |
|
0.00 |
| GOE 437 |
|
0.00 |
| GOE 438 |
|
0.00 |
| GOE 439 |
|
0.00 |
| GOE 440 |
|
0.00 |
| GOE 441 |
|
0.00 |
| GOE 442 |
|
0.00 |
| GOE 443 |
|
0.00 |
| GOE 444 |
|
0.00 |
| GOE 445 |
|
0.00 |
| GOE 446 |
|
0.00 |
| GOE 447 |
|
0.00 |
| GOE 448 |
|
0.00 |
| GOE 449 |
|
0.00 |
| GOE 450 |
|
0.00 |
| GOE 451 |
|
0.00 |
| GOE 456 |
|
0.00 |
| GOE 457 |
|
0.00 |
| GOE 458 |
|
0.00 |
| GOE 459 |
|
0.00 |
| GOE 460 |
|
0.00 |
| GOE 462 |
|
0.00 |
| GOE 464 |
|
0.00 |
| GOE 474 |
|
0.00 |
| GOE 476 |
|
0.00 |
| GOE 477 |
|
0.00 |
| GOE 478 |
|
0.00 |
| GOE 479 |
|
0.00 |
| GOE 480 |
|
0.00 |
| GOE 481 |
|
0.00 |
| GOE 481A |
|
0.00 |
| GOE 482 |
|
0.00 |
| GOE 483 |
|
0.00 |
| GOE 484 |
|
0.00 |
| GOE 488 |
|
0.00 |
| GOE 490 |
|
0.00 |
| GOE 491 |
|
0.00 |
| GOE 492 |
|
0.00 |
| GOE 493 |
|
0.00 |
| GOE 494 |
|
0.00 |
| GOE 495 |
|
0.00 |
| GOE 496 |
|
0.00 |
| GOE 497 |
|
0.00 |
| GOE 498 |
|
0.00 |
| GOE 499 |
|
0.00 |
| GOE 500 |
|
0.00 |
| GOE 501 |
|
0.00 |
| GOE 502 |
|
0.00 |
| GOE 503 |
|
0.00 |
| GOE 504 |
|
0.00 |
| GOE 505 |
|
0.00 |
| GOE 506 |
|
0.00 |
| GOE 507 |
|
0.00 |
| GOE 508 |
|
0.00 |
| GOE 509 |
|
0.00 |
| GOE 510 |
|
0.00 |
| GOE 511 |
|
0.00 |
| GOE 512 |
|
0.00 |
| GOE 513 |
|
0.00 |
| GOE 514 |
|
0.00 |
| GOE 515 |
|
0.00 |
| GOE 517 |
|
0.00 |
| GOE 518 |
|
0.00 |
| GOE 522 |
|
0.00 |
| GOE 523 |
|
0.00 |
| GOE 525 |
|
0.00 |
| GOE 526 |
|
0.00 |
| GOE 527 |
|
0.00 |
| GOE 528 |
|
0.00 |
| GOE 529 |
|
0.00 |
| GOE 530 |
|
0.00 |
| GOE 531 |
|
0.00 |
| GOE 532 |
|
0.00 |
| GOE 533 |
|
0.00 |
| GOE 534 |
|
0.00 |
| GOE 535 |
|
0.00 |
| GOE 54 |
|
0.00 |
| GOE 546 |
|
0.00 |
| GOE 547 |
|
0.00 |
| GOE 548 |
|
0.00 |
| GOE 549 |
|
0.00 |
| GOE 55 |
|
0.00 |
| GOE 550 |
|
0.00 |
| GOE 553 |
|
0.00 |
| GOE 559 |
|
0.00 |
| GOE 561 |
|
0.00 |
| GOE 562 |
|
0.00 |
| GOE 563 |
|
0.00 |
| GOE 564 |
|
0.00 |
| GOE 565 |
|
0.00 |
| GOE 566 |
|
0.00 |
| GOE 567 |
|
0.00 |
| GOE 57 |
|
0.00 |
| GOE 570 |
|
0.00 |
| GOE 571 |
|
0.00 |
| GOE 572 |
|
0.00 |
| GOE 573 |
|
0.00 |
| GOE 574 |
|
0.00 |
| GOE 575 |
|
0.00 |
| GOE 584 |
|
0.00 |
| GOE 585 |
|
0.00 |
| GOE 587 |
|
0.00 |
| GOE 590 |
|
0.00 |
| GOE 591 |
|
0.00 |
| GOE 592 |
|
0.00 |
| GOE 593 |
|
0.00 |
| GOE 595 |
|
0.00 |
| GOE 596 |
|
0.00 |
| GOE 598 |
|
0.00 |
| GOE 599 |
|
0.00 |
| GOE 5K |
|
0.00 |
| GOE 600 |
|
0.00 |
| GOE 601 |
|
0.00 |
| GOE 602 |
|
0.00 |
| GOE 602 MOD. |
|
0.00 |
| GOE 604 |
|
0.00 |
| GOE 610 B |
|
0.00 |
| GOE 610-B MOD. |
|
0.00 |
| GOE 611 |
|
0.00 |
| GOE 612 |
|
0.00 |
| GOE 613 |
|
0.00 |
| GOE 614 |
|
0.00 |
| GOE 615 |
|
0.00 |
| GOE 617 |
|
0.00 |
| GOE 619 |
|
0.00 |
| GOE 620 |
|
0.00 |
| GOE 621 |
|
0.00 |
| GOE 622 |
|
0.00 |
| GOE 623 |
|
0.00 |
| GOE 624 |
|
0.00 |
| GOE 625 |
|
0.00 |
| GOE 626 |
|
0.00 |
| GOE 627 |
|
0.00 |
| GOE 628 |
|
0.00 |
| GOE 629 |
|
0.00 |
| GOE 63 |
|
0.00 |
| GOE 630 |
|
0.00 |
| GOE 632 |
|
0.00 |
| GOE 633 |
|
0.00 |
| GOE 645 |
|
0.00 |
| GOE 646 |
|
0.00 |
| GOE 647 |
|
0.00 |
| GOE 648 |
|
0.00 |
| GOE 650 |
|
0.00 |
| GOE 652 |
|
0.00 |
| GOE 654 |
|
0.00 |
| GOE 655 |
|
0.00 |
| GOE 670 |
|
0.00 |
| GOE 673 |
|
0.00 |
| GOE 675 |
|
0.00 |
| GOE 676 (= M 12) |
|
0.00 |
| GOE 677 (= M 6) |
|
0.00 |
| GOE 679 |
|
0.00 |
| GOE 681 |
|
0.00 |
| GOE 682 |
|
0.00 |
| GOE 683 |
|
0.00 |
| GOE 685 |
|
0.00 |
| GOE 692 |
|
0.00 |
| GOE 693 |
|
0.00 |
| GOE 6K |
|
0.00 |
| GOE 701 |
|
0.00 |
| GOE 702 |
|
0.00 |
| GOE 703 |
|
0.00 |
| GOE 704 |
|
0.00 |
| GOE 711 |
|
0.00 |
| GOE 723 |
|
0.00 |
| GOE 735 |
|
0.00 |
| GOE 738 |
|
0.00 |
| GOE 741 |
|
0.00 |
| GOE 744 |
|
0.00 |
| GOE 746 |
|
0.00 |
| GOE 758 |
|
0.00 |
| GOE 766 |
|
0.00 |
| GOE 767 |
|
0.00 |
| GOE 769 |
|
0.00 |
| GOE 770 |
|
0.00 |
| GOE 775 |
|
0.00 |
| GOE 776 |
|
0.00 |
| GOE 777 |
|
0.00 |
| GOE 780 |
|
0.00 |
| GOE 79 (PFALZ 11) |
|
0.00 |
| GOE 795 |
|
0.00 |
| GOE 795 SMOOTHED |
|
0.00 |
| GOE 796 |
|
0.00 |
| GOE 797 |
|
0.00 |
| GOE 798 |
|
0.00 |
| GOE 7K |
|
0.00 |
| GOE 801 (MVA 301) |
|
0.00 |
| GOE 802 |
|
0.00 |
| GOE 802 A |
|
0.00 |
| GOE 802 B |
|
0.00 |
| GOE 803 (HACKLINGER) |
|
0.00 |
| GOE 804 (EA 8) |
|
0.00 |
| GOE 81 |
|
0.00 |
| GOE 8K |
|
0.00 |
| GOE 92 |
|
0.00 |
| GOE 9K |
|
0.00 |
| GOE-796 |
|
12.00 |
| GOT-398 |
|
13.85 |
| GOT-409 |
|
12.70 |
| GOT-411 |
|
13.20 |
| GOT-417 |
|
6.00 |
| GOT-420 |
|
18.75 |
| GOT-436 |
|
11.00 |
| GOT-439 |
Pour planeur de thermique |
8.00 |
| GOT-445 |
|
6.40 |
| GOT-449 |
|
17.20 |
| GOT-459 |
|
12.70 |
| GOT-496 |
|
9.95 |
| GOT-497 |
|
12.70 |
| GOT-500 |
|
10.00 |
| GOT-532 |
|
12.50 |
| GOT-533 |
|
13.70 |
| GOT-535 |
|
16.05 |
| GOT-546 |
|
10.40 |
| GOT-549 |
|
13.85 |
| GOT-564 |
|
8.20 |
| GOT-591 |
|
11.20 |
| GOT-593 |
|
12.00 |
| GOT-596 |
|
9.75 |
| GOT-602 |
|
9.95 |
| GOT-602M |
|
9.60 |
| GOT-612 |
|
10.40 |
| GOT-613 |
|
10.30 |
| GOT-622 |
|
8.00 |
| GOT-623 |
|
12.00 |
| GOT-625 |
|
20.00 |
| GOT-632 |
|
14.00 |
| GOT-655 |
|
13.90 |
| GOT-676 |
|
11.90 |
| GOT-682 |
|
10.65 |
| GOT-693 |
|
12.00 |
| GOT-795 |
|
8.00 |
| GOT-801 |
|
9.80 |
| GOTTINGEN 155 |
|
|
| GOTTINGEN 409 |
|
|
| GOTTINGEN 410 |
|
|
| GOTTINGEN 411 |
|
|
| GOTTINGEN 436 |
|
|
| GOTTINGEN 459 |
|
|
| GOTTINGEN 508 |
|
|
| GOTTINGEN 532 |
|
|
| GOTTINGEN 533 |
|
13.70 |
| GOTTINGEN 535 |
|
16.00 |
| GOTTINGEN 549 |
|
14.00 |
| GOTTINGEN 565 |
|
|
| GOTTINGEN 593 |
|
|
| GOTTINGEN 598 |
|
|
| GOTTINGEN 600 |
|
|
| GOTTINGEN 601 |
|
|
| GOTTINGEN 602 |
|
|
| GOTTINGEN 611 |
|
|
| GOTTINGEN 623 |
|
|
| GOTTINGEN 676 |
|
|
| GOTTINGEN 677 |
|
|
| GOTTINGEN 693 |
|
12.00 |
| GOTTINGEN 766 |
|
12.00 |
| GOTTINGEN 795 |
|
|
| GOTTINGEN 796 |
|
|
| GOTTINGEN 797 |
|
|
| Griffith |
thick symmetrical suction airfoil (approximate coordinates taken from Fig. 1 R&M 2149 |
0.00 |
| GRUMMAN K-2 |
|
0.00 |
| GRUMMAN K-3 |
|
0.00 |
| H.S. 1.7/9 |
|
9.00 |
| HAWKER TEMPEST 37.5% SEMISPAN |
|
37.50 |
| HAWKER TEMPEST 61% SEMISPAN |
|
61.00 |
| HAWKER TEMPEST 96.77% SEMISPAN |
|
96.77 |
| HL 74-3512 |
|
|
| HL 80-13353 |
|
|
| HL743512 |
|
11.90 |
| HL753308 |
|
8.15 |
| HL801335 |
Profil polyvalent du planeur de vol de pente a l'avion de voltige |
13.40 |
| HL813353 |
|
13.45 |
| HN85-2-9 |
|
9.16 |
| HOBIE |
|
0.00 |
| HOBIESMO1.DAT |
|
0.00 |
| HORSTMANN AND QUAST HQ-300 GD(MOD 2) |
|
0.00 |
| HORT-10 |
|
10.00 |
| HORT-50 |
|
10.00 |
| HORT-II |
Profil pour aile volante a utiliser avec le Horten standart |
10.00 |
| HORT-ST |
Profil pour aile volante a utiliser avec le Horten II |
13.00 |
| HQ 0/10 |
|
10.00 |
| HQ 0/7 |
|
7.00 |
| HQ 0/9 |
|
9.00 |
| HQ 1.0/10 |
|
10.00 |
| HQ 1.0/12 |
|
12.00 |
| HQ 1.5/10 |
|
10.00 |
| HQ 1.5/11 |
|
11.00 |
| HQ 1.5/12 |
|
12.00 |
| HQ 1.5/8 |
|
8.00 |
| HQ 1.5/8.5 |
|
8.50 |
| HQ 1.5/9 |
|
9.00 |
| HQ 1.5/9 B |
|
9.00 |
| HQ 1/10 |
|
10.00 |
| HQ 1/8 |
|
8.00 |
| HQ 1/9 |
|
9.00 |
| HQ 2./10 |
|
10.00 |
| HQ 2./12 |
|
12.00 |
| HQ 2./8 |
|
8.00 |
| HQ 2./9 |
|
9.00 |
| HQ 2.1/9.5 |
|
9.50 |
| HQ 2.5/10 |
|
10.00 |
| HQ 2.5/11 |
|
11.00 |
| HQ 2.5/12 |
|
12.00 |
| HQ 2.5/8 |
|
8.00 |
| HQ 2.5/9 |
|
9.00 |
| HQ 2.5/9 B |
|
9.00 |
| HQ 2.5/9.0 SMOOTHED BY EPPLER |
|
9.00 |
| HQ 3.0/10 |
|
10.00 |
| HQ 3.0/11 |
|
11.00 |
| HQ 3.0/13 |
|
13.00 |
| HQ 3.0/14 |
|
14.00 |
| HQ 3.0/15 |
|
15.00 |
| HQ 3.0/8 |
|
8.00 |
| HQ 3.0/9 |
|
9.00 |
| HQ 3.5/10 |
|
10.00 |
| HQ 3.5/12 |
|
12.00 |
| HQ 3.5/13 |
|
13.00 |
| HQ 3.5/14 |
|
14.00 |
| HQ 3.5/18 |
|
18.00 |
| HQ 3.5/8 |
|
8.00 |
| HQ 3.5/9 |
|
9.00 |
| HQ 3/12 |
|
12.00 |
| HQ-0-10 |
|
10.00 |
| HQ-0-9 |
|
8.11 |
| HQ-10-08 |
|
8.00 |
| HQ-10-09 |
|
9.00 |
| HQ-10-10 |
|
10.00 |
| HQ-10-12 |
|
12.00 |
| HQ-15-08 |
|
7.99 |
| HQ-15-09 |
|
8.98 |
| HQ-15-10 |
|
10.00 |
| HQ-15-11 |
|
11.00 |
| HQ-15-12 |
|
12.00 |
| HQ-15-85 |
|
8.55 |
| HQ-2.0/9 9.0% SMOOTHED |
|
9.00 |
| HQ-20-08 |
|
8.00 |
| HQ-20-09 |
|
8.98 |
| HQ-20-10 |
|
10.00 |
| HQ-20-11 |
|
11.00 |
| HQ-20-12 |
|
12.00 |
| HQ-20-14 |
|
14.00 |
| HQ-21-95 |
|
9.49 |
| HQ-25-08 |
|
8.00 |
| HQ-25-09 |
|
8.98 |
| HQ-25-10 |
|
10.00 |
| HQ-25-11 |
|
11.00 |
| HQ-25-12 |
|
12.00 |
| HQ-25-9B |
|
9.03 |
| HQ-30-08 |
|
8.00 |
| HQ-30-09 |
|
9.00 |
| HQ-30-10 |
|
10.00 |
| HQ-30-11 |
|
11.00 |
| HQ-30-12 |
|
12.00 |
| HQ-30-13 |
|
13.00 |
| HQ-30-14 |
|
14.00 |
| HQ-30-15 |
|
15.00 |
| HQ-35-08 |
|
8.00 |
| HQ-35-09 |
|
9.00 |
| HQ-35-10 |
|
10.00 |
| HQ-35-12 |
|
12.00 |
| HQ-35-14 |
|
14.00 |
| HQ-35-18 |
|
18.00 |
| HQ/W-2-8 |
|
8.00 |
| HQ1008GL |
|
7.97 |
| HQ1009GL |
|
8.98 |
| HQ1010GL |
|
9.96 |
| HQ1012GL |
|
11.95 |
| HQ1508GL |
|
7.95 |
| HQ1509GL |
|
8.96 |
| HQ1510GL |
|
9.96 |
| HQ1512GL |
|
11.95 |
| HQ2008GL |
|
7.97 |
| HQ2009GL |
|
8.97 |
| HQ2010GL |
|
9.97 |
| HQ2012GL |
|
11.97 |
| HQ2508GL |
|
7.96 |
| HQ2509GL |
|
8.96 |
| HQ2510GL |
|
9.96 |
| HQ2512GL |
|
11.96 |
| HQ3008GL |
|
7.97 |
| HQ3009GL |
|
8.97 |
| HQ3010GL |
|
9.98 |
| HQ3011GL |
|
10.98 |
| HQ3012GL |
|
11.98 |
| HQ3013GL |
|
12.98 |
| HQ3014GL |
|
13.98 |
| HQ3015GL |
|
14.98 |
| HQ3508GL |
|
7.96 |
| HQ3509GL |
|
8.97 |
| HQ3510GL |
|
9.96 |
| HQ3512GL |
|
11.95 |
| HQN-1585 |
|
8.55 |
| HS-17-9 |
Profil performant pour comptition F3B |
9.00 |
| HSNLF(1)-0213 |
|
0.00 |
| HUGHES HELICOPTERS HH-02 |
|
0.00 |
| J-5012 |
|
12.00 |
| J5012 12% |
|
12.00 |
| JGM4-126 |
|
6.00 |
| JN-153 |
|
0.00 |
| JOUKOWSKI |
|
12.00 |
| JPM3-07 |
|
10.13 |
| K3311 (ORIGINAL) |
|
0.00 |
| K3311 (SMOOTHED) |
|
0.00 |
| KC-135 BL124.32 |
|
0.00 |
| KC-135 BL200.76 |
|
0.00 |
| KC-135 BL351.6 |
|
0.00 |
| KC-135 BL52.44 |
|
0.00 |
| KENNEDY AND MARSDEN |
|
0.00 |
| KOSTER66 |
|
6.75 |
| LA 203 A |
|
15.75 |
| LINDNER2 |
|
6.65 |
| LISS. 7769 |
|
10.99 |
| LISS7769 |
|
10.98 |
| LNV109A |
|
0.00 |
| LOCKHEED C-141 BL0 |
|
0.00 |
| LOCKHEED C-141 BL113.6 |
|
0.00 |
| LOCKHEED C-141 BL426.57 |
|
0.00 |
| LOCKHEED C-141 BL610.61 |
|
0.00 |
| LOCKHEED C-141 BL761.11 |
|
0.00 |
| LOCKHEED C-141 BL958.89 |
|
0.00 |
| LOCKHEED C-5A BL0 |
|
0.00 |
| LOCKHEED C-5A BL1256 |
|
0.00 |
| LOCKHEED C-5A BL488.2 |
|
0.00 |
| LOCKHEED C-5A BL576 |
|
0.00 |
| LOCKHEED C-5A BL758.6 |
|
0.00 |
| LOCKHEED L-188 ROOT |
|
0.00 |
| LOCKHEED L-188 TIP |
|
0.00 |
| LOCKHEED-GEORGIA SUPERCRITICAL |
|
0.00 |
| LRN1007 |
|
0.00 |
| LS1-0416 |
|
16.06 |
| MA 409 |
|
6.79 |
| MA409 (ORIGINAL) |
|
0.00 |
| MA409 (SMOOTHED) |
|
0.00 |
| MARSDEN |
|
0.00 |
| MARSKE MONARCH |
(NACA 43012A) |
0.00 |
| MARSKE PIONEER IA |
(NACA 23112/43012A HYBRID) |
0.00 |
| MARSKE PIONEER IID ROOT |
(NACA 431012A/24112 HYBRID) |
0.00 |
| MARSKE PIONEER IID TIP |
(NACA 431012A*.833 HYBRID) |
0.00 |
| MARSKE XM-1D |
|
0.00 |
| MB253515 |
Profil utilisable de l'avion au F3B - centrage 30
32% |
15.00 |
| MB253515 15.0% SMOOTHED |
|
15.00 |
| MFE-P 205.925 (K 22.5) |
|
|
| MFE20592 |
Profil pour planeur de pente ou lectrique |
9.25 |
| MH 18 |
|
11.13 |
| MH 18 (11.14%) |
|
11.14 |
| MH 20 |
|
9.02 |
| MH 20 (9.02%) |
|
9.02 |
| MH 22 (7.21 %) |
|
7.21 |
| MH 30 |
|
7.84 |
| MH 42 (8.94 %) |
FUN AND SLOPE SOARING, PRE-F3B (CL(CD_MIN)=0.2) |
8.90 |
| MH 43 (8.50 %) |
PYLON RACING, SMALL ELECTRIC POWERED MODELS CM0 = -.022 |
8.50 |
| MH 46 |
|
11.27 |
| MH 49 |
|
10.49 |
| MH 60 (10.08 %) |
|
10.08 |
| MH 61 (10.28 %) |
|
10.28 |
| MH 62 (9.30 %) |
|
9.30 |
| MH 64 |
|
8.57 |
| MH-18 |
|
11.05 |
| MH-20 |
Pour avion très rapide style course aux pylône |
9.00 |
| MH-22 |
|
7.00 |
| MH-32 |
|
8.71 |
| MH-42 |
|
9.00 |
| MH-43-0 |
|
8.50 |
| MH-60 |
|
10.00 |
| MH-61 |
|
10.25 |
| MH-62 |
|
9.22 |
| MH-64 |
|
8.53 |
| MH32 (8.71%) |
|
8.71 |
| MH45 |
|
0.00 |
| MILEY M06-13-128 |
|
0.00 |
| MVA-173 |
|
7.70 |
| MVA-301 |
Pour planeur thermique lent |
10.00 |
| N-22 |
|
12.30 |
| N-60 |
|
12.37 |
| N-7 |
|
6.65 |
| N-9 |
|
8.46 |
| N2311275 |
|
12.22 |
| N60R |
Pour avion type remorqeur ou maquette |
12.40 |
| N631-012 |
|
12.00 |
| N631-412 |
|
12.00 |
| N631A012 |
|
11.99 |
| N631A412 |
|
11.99 |
| N631A512 |
|
11.99 |
| N631A612 |
|
11.99 |
| N63A-010 |
|
9.99 |
| N641A012 |
|
11.98 |
| N651-012 |
|
11.99 |
| N652-015 |
|
14.99 |
| NA23009 |
|
9.08 |
| NA23012 |
|
12.06 |
| NA23015 |
|
15.04 |
| NA23112 |
|
12.22 |
| NA25411 |
|
10.99 |
| NA2R112 |
Pour planeur et avion de voltige |
12.00 |
| NA63-009 |
|
8.89 |
| NA63-010 |
|
9.87 |
| NA63-206 |
|
6.00 |
| NA63-209 |
|
9.00 |
| NA63-210 |
|
10.00 |
| NA63-415 |
|
15.00 |
| NA633018 |
derive du tigre |
0.97 |
| NA633618 |
|
18.61 |
| NA634412 |
Profil pour grand planeur - centrage de 34
36% |
12.00 |
| NA63A006 |
|
5.97 |
| NA63A008 |
Profil pour stabilisateur |
8.00 |
| NA63A012 |
|
12.00 |
| NA63A408 |
|
8.00 |
| NA63A410 |
|
10.00 |
| NA63A411 |
|
10.99 |
| NA63A412 |
|
12.00 |
| NA63A413 |
|
12.99 |
| NA63A414 |
|
13.98 |
| NA63A510 |
|
9.99 |
| NA63A511 |
|
10.99 |
| NA63A513 |
|
12.99 |
| NA63A514 |
|
13.98 |
| NA63A608 |
|
8.00 |
| NA63A610 |
|
10.00 |
| NA63A611 |
|
10.99 |
| NA63A612 |
|
12.00 |
| NA63A613 |
|
12.99 |
| NA63A614 |
|
13.98 |
| NA64-006 |
|
5.98 |
| NA64-009 |
|
8.98 |
| NA64-010 |
|
9.97 |
| NA64-012 |
|
12.00 |
| NA64015 |
Profil pour la voltige moderne avion |
15.00 |
| NA641012 |
|
11.96 |
| NA641112 |
|
9.97 |
| NA643618 |
|
18.00 |
| NA64A010 |
|
9.99 |
| NA64A610 |
|
10.00 |
| NA65-009 |
|
8.99 |
| NA65-010 |
|
9.99 |
| NA653018 |
|
18.00 |
| NA653019 |
|
19.00 |
| NA654415 |
|
15.00 |
| NA66-116 |
|
15.99 |
| NACA 0009 |
|
9.00 |
| NACA 0012 |
|
|
| NACA 0015 |
|
|
| NACA 0018 |
|
|
| NACA 006 |
|
0.00 |
| NACA 1-H-15 |
|
0.00 |
| NACA 11-H-09 |
|
0.00 |
| NACA 1410 |
|
10.00 |
| NACA 2-H-15 |
|
0.00 |
| NACA 2.5411 |
|
0.00 |
| NACA 20-32C |
|
0.00 |
| NACA 2212 |
|
|
| NACA 23012 |
|
12.00 |
| NACA 23012 12% |
|
12.00 |
| NACA 23015 |
|
|
| NACA 2409 |
|
0.00 |
| NACA 2412 |
|
12.00 |
| NACA 2414 |
|
0.00 |
| NACA 2415 |
Biconvexe dissymétriqueAvions de transition à ailerons.Calage entre 0° et 1.5°.Centrage entre 28% et 33% |
|
| NACA 2512 |
|
|
| NACA 2R2-12 |
|
|
| NACA 4409 |
|
0.00 |
| NACA 4410 |
|
|
| NACA 4412 |
|
12.00 |
| NACA 4415 |
Profil Plat |
|
| NACA 5-H-10 |
|
0.00 |
| NACA 5-H-15 |
|
0.00 |
| NACA 5-H-20 |
|
0.00 |
| NACA 6-H-10 |
|
0.00 |
| NACA 6-H-15 |
|
0.00 |
| NACA 6-H-20 |
|
0.00 |
| NACA 63 010 |
|
|
| NACA 63 3 618 |
|
|
| NACA 63 A 108 |
|
|
| NACA 63 A 110 |
|
|
| NACA 63 A 210 |
|
|
| NACA 63 A 408 |
|
|
| NACA 63 A 410 |
|
10.00 |
| NACA 63 A 412 |
|
|
| NACA 63 A 608 |
|
|
| NACA 63 A 610 |
|
|
| NACA 63 A 612 |
|
12.00 |
| NACA 63(2)-215 MOD B |
|
0.00 |
| NACA 63-015A |
|
0.00 |
| NACA 63-210 |
|
0.00 |
| NACA 63-212 |
|
0.00 |
| NACA 63-215 |
|
0.00 |
| NACA 63-412 |
|
0.00 |
| NACA 63012A |
|
0.00 |
| NACA 63212 |
|
|
| NACA 63415 |
|
|
| NACA 63A 418 |
|
|
| NACA 63A 518 |
|
|
| NACA 63A010 |
|
0.00 |
| NACA 64 1 212 |
|
|
| NACA 64 20.5 10 |
|
|
| NACA 64 3 618 |
|
|
| NACA 64 30 10 |
|
|
| NACA 64 30.5 10 |
|
|
| NACA 64 31 10 |
|
|
| NACA 64 A 210 |
|
|
| NACA 64 A 410 |
|
|
| NACA 64 A 610 |
|
|
| NACA 64(1)-212 |
|
0.00 |
| NACA 64(1)-212 MOD A |
|
0.00 |
| NACA 64(1)-212 MOD B |
|
0.00 |
| NACA 64-008A |
|
0.00 |
| NACA 64-012A |
|
0.00 |
| NACA 64-108 |
|
0.00 |
| NACA 64-110 |
|
0.00 |
| NACA 64-215 |
|
0.00 |
| NACA 6409 |
|
9.00 |
| NACA 6412 |
|
|
| NACA 642-015 |
|
0.00 |
| NACA 642-015A |
|
0.00 |
| NACA 64412 |
|
|
| NACA 64A-010 10.0% |
|
10.00 |
| NACA 65 015 |
|
|
| NACA 65212 |
|
|
| NACA 65412 |
|
|
| NACA 65415 |
|
|
| NACA 66 |
|
|
| NACA 66,2-(1.8)12 A=.6 P-51 TIP |
|
0.00 |
| NACA 66,2-(1.8)15.5 A=.6 P-51 ROOT |
|
0.00 |
| NACA 66-018 |
|
0.00 |
| NACA 66-021 |
|
0.00 |
| NACA 8-H-12 |
|
0.00 |
| NACA CYH |
|
|
| NACA M1 |
|
|
| NACA M10 |
|
0.00 |
| NACA M11 |
|
0.00 |
| NACA M12 |
|
0.00 |
| NACA M13 |
|
0.00 |
| NACA M14 |
|
0.00 |
| NACA M15 |
|
0.00 |
| NACA M16 |
|
0.00 |
| NACA M17 |
|
0.00 |
| NACA M18 |
|
0.00 |
| NACA M19 |
|
0.00 |
| NACA M2 |
|
0.00 |
| NACA M20 |
|
0.00 |
| NACA M21 |
|
0.00 |
| NACA M22 |
|
0.00 |
| NACA M23 |
|
0.00 |
| NACA M24 |
|
0.00 |
| NACA M25 |
|
0.00 |
| NACA M26 |
|
0.00 |
| NACA M27 |
|
0.00 |
| NACA M3 |
|
|
| NACA M4 |
|
0.00 |
| NACA M5 |
|
0.00 |
| NACA M6 |
|
0.00 |
| NACA M7 |
|
0.00 |
| NACA M8 |
|
0.00 |
| NACA M9 |
|
0.00 |
| NACA-0009 9.0% SMOOTHED |
|
9.00 |
| NACA-M1 |
|
0.00 |
| NACA-M3 |
|
12.00 |
| NACA/LANGLEY SYMMETRICAL, SUPERCRITICAL |
|
0.00 |
| NACA0008 |
|
8.00 |
| NACA0009 |
|
9.00 |
| NACA0010 |
|
10.00 |
| NACA0012 |
|
12.00 |
| NACA1408 |
|
8.46 |
| NACA1410 |
|
10.00 |
| NACA1412 |
|
12.00 |
| NACA2408 |
|
8.00 |
| NACA2409 |
|
9.00 |
| NACA2410 |
|
10.00 |
| NACA2412 |
Utilisable du petit planeur
l'avion - centrage 28
31% |
12.00 |
| NACA2415 |
|
15.00 |
| NACA2512 |
|
12.02 |
| NACA2515 |
|
15.00 |
| NACA4309 |
|
9.00 |
| NACA4409 |
|
9.00 |
| NACA4412 |
|
12.00 |
| NACA4415 |
Pour avion type petit gros |
15.00 |
| NACA4418 |
|
18.00 |
| NACA6409 |
|
9.00 |
| NACA6409 9% |
|
9.00 |
| NACA6412 |
|
12.00 |
| NASA NLF1015 |
|
0.00 |
| NASA RC(4)-10 |
|
0.00 |
| NASA RC(5)-10 |
|
0.00 |
| NASA/AMES 63A108 MOD C |
|
0.00 |
| NASA/AMES A-01 |
|
0.00 |
| NASA/AMES A-02 |
|
0.00 |
| NASA/AMES A-03 |
|
0.00 |
| NASA/LANGLEY 64-012 |
|
0.00 |
| NASA/LANGLEY LS(1)-0013 |
|
0.00 |
| NASA/LANGLEY LS(1)-0413 (GA(W)-2) |
|
0.00 |
| NASA/LANGLEY LS(1)-0413MOD |
|
0.00 |
| NASA/LANGLEY LS(1)-0417 (GA(W)-1) |
|
0.00 |
| NASA/LANGLEY LS(1)-0417MOD |
|
0.00 |
| NASA/LANGLEY LS(1)-0421 |
|
0.00 |
| NASA/LANGLEY LS(1)-0421MOD |
|
0.00 |
| NASA/LANGLEY MS(1)-0317 |
|
0.00 |
| NASA/LANGLEY MS(1)-0413 |
|
0.00 |
| NASA/LANGLEY NLF 0414F |
|
0.00 |
| NASA/LANGLEY NLF(1)-0215F |
|
0.00 |
| NASA/LANGLEY NLF(1)-0416 |
|
0.00 |
| NASA/LANGLEY NLF(2)-0415 |
|
0.00 |
| NASA/LANGLEY RC-08(B)3 |
|
0.00 |
| NASA/LANGLEY RC-08(N)1 |
|
0.00 |
| NASA/LANGLEY RC-10(B)3 |
|
0.00 |
| NASA/LANGLEY RC-10(N)1 |
|
0.00 |
| NASA/LANGLEY RC-12(B)3 |
|
0.00 |
| NASA/LANGLEY RC-12(N)1 |
|
0.00 |
| NASA/LANGLEY RC-SC2 |
|
0.00 |
| NASA/LANGLEY RC08-64C |
|
0.00 |
| NASA/LANGLEY RC10-64C |
|
0.00 |
| NASA/LANGLEY RC12-64C |
|
0.00 |
| NASA/LANGLEY SC(2)-0714 SUPERCRITICAL |
|
0.00 |
| NCEP1010 |
|
9.99 |
| NCEP1510 |
|
9.99 |
| NCEP1511 |
|
10.99 |
| NCEP2010 |
|
9.99 |
| NCEP2011 |
|
10.99 |
| NCEP2012 |
|
11.99 |
| NCEP2510 |
|
9.99 |
| NCEP2511 |
|
10.99 |
| NCEP2512 |
|
11.99 |
| NCEP3010 |
|
9.99 |
| NCEP3011 |
|
10.99 |
| NCEP3012 |
|
11.99 |
| NCEP3511 |
|
10.99 |
| NCEP3512 |
|
11.99 |
| NCEP4012 |
|
11.99 |
| NLF(1)-0115 |
|
0.00 |
| NLR-1T |
|
0.00 |
| NLR-7223-43 |
|
0.00 |
| NLR-7223-62 |
|
0.00 |
| NLR-7301 |
|
0.00 |
| NON DOCUMENTÉ |
|
|
| NPL |
|
0.00 |
| NPL 9510 |
|
0.00 |
| NPL 9615 |
|
0.00 |
| NPL 9626 |
|
0.00 |
| NPL 9627 |
|
0.00 |
| NPL 9660 |
|
0.00 |
| NYU/GRUMMAN K-1 |
|
0.00 |
| OAF095 |
|
0.00 |
| OAF102 |
|
0.00 |
| OAF117 |
|
0.00 |
| OAF128 |
|
0.00 |
| OAF139 |
|
0.00 |
| ONERA NACA CAMBRE |
|
0.00 |
| ONERA OA206 |
|
0.00 |
| ONERA OA209 |
|
0.00 |
| ONERA OA212 |
|
0.00 |
| ONERA OA213 |
|
0.00 |
| ORNITHOPTER AIRFOIL. |
|
0.00 |
| P-51D ROOT (BL17.5) |
|
16.50 |
| P-51D TIP (BL215) |
|
16.50 |
| PESCOR |
|
|
| PMC19SM |
|
0.00 |
| PROFIL 374 DICKE 10.92% |
|
10.92 |
| PROFIL 387 DICKE 9.06% |
|
9.06 |
| PSU 90-125WL |
|
0.00 |
| QB-2195 |
Profil optimisé pour le F3B ou planeur rapide sauf de voltige-volets de 22% pos |
9.50 |
| R140 12.04% (SMOOTHED) |
|
12.04 |
| R140 (ORIGINAL) |
|
0.00 |
| RA163C3 |
|
16.30 |
| RA163CW3 |
|
16.30 |
| RAE 2822 |
|
0.00 |
| RAE 5214 |
|
0.00 |
| RAE 5215 |
|
0.00 |
| RAE(NPL) 5212 |
|
0.00 |
| RAE(NPL) 5213 |
|
0.00 |
| RAE6-9CK |
|
0.00 |
| RAF 15 |
|
0.00 |
| RAF 19 |
|
0.00 |
| RAF 25 |
|
0.00 |
| RAF 26 |
|
0.00 |
| RAF 27 |
|
9.70 |
| RAF 28 |
|
9.70 |
| RAF 30 |
|
0.00 |
| RAF 30 MOD |
|
0.00 |
| RAF 31 |
|
0.00 |
| RAF 32 |
|
0.00 |
| RAF 32 MOD |
|
0.00 |
| RAF 33 |
|
0.00 |
| RAF 34 |
|
0.00 |
| RAF 38 |
|
0.00 |
| RAF 6 |
|
0.00 |
| RAF 69 |
|
0.00 |
| RAF 89 |
|
0.00 |
| RAF-48 |
|
0.00 |
| RAF28 |
|
9.82 |
| RAF32 |
|
12.68 |
| REPUBLIC S-3 |
|
0.00 |
| RG 12 |
|
9.26 |
| RG 12A |
|
9.00 |
| RG 12A-1.8/9.0 |
|
0.00 |
| RG 14 |
|
8.74 |
| RG 14 10% |
|
10.00 |
| RG 14 9% |
|
9.00 |
| RG 14 9.5% |
|
9.50 |
| RG 14A-1.4/7.0 |
|
7.00 |
| RG 15 |
|
8.98 |
| RG 15A 2.5/13.0 |
|
13.00 |
| RG 15A-1.8/11.0 |
|
11.00 |
| RG 8 |
|
10.80 |
| RG 8/9 |
|
9.00 |
| RG-0008 |
|
10.80 |
| RG-12 |
|
0.00 |
| RG-12 |
|
9.27 |
| RG-12A 9.00% |
|
9.00 |
| RG-12A18 |
|
9.00 |
| RG-14 |
|
8.45 |
| RG-15 |
|
8.93 |
| RG-15A18 |
Pour le vol a voile et la pente centrage 33
35 % |
11.00 |
| RG12A189 |
|
8.98 |
| RG14A147 |
|
6.99 |
| RG15A111 |
|
11.13 |
| RG15A213 |
|
12.99 |
| RHODE ST GENESE 28 |
|
|
| RITZ 1-30-10 |
Biconvexe dissymétriqueVoltige planeurAccélère très fort.Centrage 30%.Calage 1.5° à 2.5°
|
10.00 |
| RITZ 1-30-12 |
|
|
| RITZ 2-30-10 |
Biconvexe dissymétrique. Utiliser ne grandes plumes.Permet l'exploitation de thermiques et la voltige.. Centrage 33%. Calage 2° à 3° |
10.00 |
| RITZ 2-30-12 |
Biconvexe dissymétrique. Utiliser ne grandes plumes.Permet l'exploitation de thermiques et la voltige.. Centrage 33%. Calage 2° à 3° |
|
| RITZ 3-30-10 |
|
|
| RITZ 3-30-12 |
Biconvexe dissymétrique. Utiliser ne grandes plumes.Permet l'exploitation de thermiques et la voltige.. Centrage 33%. Calage 2° à 3° |
12.00 |
| RITZ1310 |
|
9.93 |
| RITZ1312 |
|
11.93 |
| RITZ2310 |
|
9.91 |
| RITZ2312 |
|
11.91 |
| RITZ2314 |
|
13.89 |
| RITZ3310 |
|
9.91 |
| RITZ3312 |
|
11.93 |
| RITZ3314 |
|
13.91 |
| RK40 |
|
7.5 |
| RONCZ LOW DRAG FLYING WING |
|
12.05 |
| RUTAN CANARD |
|
11.60 |
| RUTAN WING |
|
11.76 |
| RYAN BQM-34 FIREBEE WING |
|
0.00 |
| S 2046-090-83 |
|
|
| S 3002-099-83 |
|
|
| S 3021 |
|
9.47 |
| S 4053-089-84 |
|
|
| S-1210 |
|
11.74 |
| S-1223 |
|
12.05 |
| S-2027 |
|
14.48 |
| S-2046 |
|
8.95 |
| S-2091 |
|
10.01 |
| S-3002 |
|
9.78 |
| S-3010 |
|
10.30 |
| S-3021 |
|
9.37 |
| S-4022 |
|
11.19 |
| S-4053 |
|
8.82 |
| S-4061 |
|
9.52 |
| S-4083 |
|
7.90 |
| S-4110 |
|
8.30 |
| S-4158 |
|
10.72 |
| S-4180 |
|
9.71 |
| S-4233 |
|
13.53 |
| S-4310 |
|
10.76 |
| S-4320 |
|
9.36 |
| S-4410 |
|
9.58 |
| S-4411 |
|
9.54 |
| S-4412 |
|
9.20 |
| S-4413 |
|
9.66 |
| S-5010 |
|
9.80 |
| S-5020 |
|
8.39 |
| S-7012 |
|
8.71 |
| S.I. 64 009 |
|
|
| S1010 HPV AIRFOIL |
|
0.00 |
| S1012 |
|
0.00 |
| S1014 |
|
0.00 |
| S1016 |
|
0.00 |
| S1046 17% (DANNY HOWELL) |
|
17.00 |
| S1048 14% (DANNY HOWELL) |
|
14.00 |
| S1091 |
|
0.00 |
| S1210 12% |
|
12.00 |
| S1221 W/O FLAP |
|
0.00 |
| S1223 |
|
12.10 |
| S1223 RTL |
|
0.00 |
| S2027 |
|
0.00 |
| S2046 |
|
0.00 |
| S2048 |
|
0.00 |
| S2050 8.93% |
|
8.93 |
| S2055 |
|
0.00 |
| S2060 8% |
|
8.00 |
| S2062 8% |
|
8.00 |
| S2091-101-83 |
|
0.00 |
| S3010-103-84 |
|
10.32 |
| S3014-095-85 |
|
0.00 |
| S3016-095-87 |
|
0.00 |
| S3021-095-84 |
|
0.00 |
| S3024 9.84% |
|
9.84 |
| S3025 9.38% |
|
9.38 |
| S4022 |
|
11.30 |
| S4053 |
|
9.00 |
| S4061-096-84 |
|
9.62 |
| S4062-095-87 |
|
9.50 |
| S4083 (8%) |
|
8.00 |
| S4110 |
|
0.00 |
| S4158 |
|
0.00 |
| S4180-098-84 |
|
0.00 |
| S4233-136-84 |
|
0.00 |
| S4310 |
|
0.00 |
| S4320 |
|
0.00 |
| S5010 |
|
0.00 |
| S5010-98 |
|
9.80 |
| S5020 |
|
0.00 |
| S5020-84 |
|
8.39 |
| S6061 9% |
|
8.96 |
| S6062 8% |
|
7.83 |
| S6063 7.05% |
|
7.05 |
| S7012 8.75% |
|
8.75 |
| S7055 (10.5%) FLAT-BOTTOMED |
|
10.50 |
| S7075 (9%) |
|
8.97 |
| S8025 (8%) |
|
7.98 |
| S8035 FOR RC AEROBATIC 14% THICK |
|
14.00 |
| S8036 (16%) |
|
16.00 |
| S8037 (16%) |
|
16.00 |
| S8038 (13%) |
|
13.00 |
| S8052 (11.88%) |
|
11.90 |
| S8055 (12%) |
|
12.00 |
| SARATOV |
|
0.00 |
| SB13-X |
|
10.63 |
| SB95 10,5/2 |
Permet de gratter honorablement, d'aller vite, de tenir confortablement sur le dos d'obtenir une voltige très coulée |
10.50 |
| SB95 11,5/2 |
Permet de gratter honorablement, d'aller vite, de tenir confortablement sur le dos d'obtenir une voltige très coulée |
11.50 |
| SB95 9,5/2 |
Permet de gratter honorablement, d'aller vite, de tenir confortablement sur le dos d'obtenir une voltige très coulée |
9.50 |
| SB96 10/5.3 |
|
10.50 |
| SB96 10/5.3 |
Cz max très élevé tout en concservant une bonne finesse Orienté vol thermique |
10.50 |
| SB96 11/6.3 |
Cz max très élevé tout en concservant une bonne finesse Orienté vol thermique |
11.60 |
| SB96 11/6.3 |
|
11.60 |
| SB96 12/7.3 |
|
12.70 |
| SB96 LM |
Gratteur, pénétrant, assez facile à réaliser s'adapte aux lancer-main et aux petits motoplaneurs de durée |
8.00 |
| SB96 MU |
Modification du RG 15 très bon en F3F |
8.50 |
| SB96 V |
Voltige |
9.35 |
| SB96 VS |
Voltige pour des envergures de 2.3 à 2.5 m Gratte bien sans volets Figures à base de déclenchés nettes, sans tendance à l'ettouffement |
9.75 |
| SB97 8/1.25 |
Adapté aux racers motorisés Très bonnes accélérations et virages serrés |
8.00 |
| SB97 EP |
|
9.20 |
| SB97 EP |
Alternative au RG12A Excelle en gratte et en vitesse Bonne tenue sur le dos |
9.20 |
| SB97 FW |
Cm0 pratiquement nul et un bon Cz max Pour Ailes volantes (D-Clic) |
8.93 |
| SB98VM5 |
|
|
| SB98VR5 |
|
|
| SB98VS5 |
|
|
| SB99F3J |
|
|
| SC(2)-0714 SUPERCRITICAL AIRFOIL |
Supercritical airfoil (coordinates from Raymer w/ one correction) |
0.00 |
| SD2030 |
|
8.49 |
| SD2030-086-88 |
|
0.00 |
| SD2083 (9.0%) |
|
9.00 |
| SD5060 |
|
9.45 |
| SD5060 (9.5%) |
|
9.50 |
| SD6060 |
|
10.35 |
| SD6060-104-88 |
|
0.00 |
| SD6080 |
|
9.07 |
| SD6080 (9.2%) |
|
9.20 |
| SD7003 |
|
8.49 |
| SD7003-085-88 |
|
0.00 |
| SD7032 |
|
9.90 |
| SD7032-099-88 |
|
0.00 |
| SD7034 |
|
0.00 |
| SD7037 |
|
9.11 |
| SD7037-092-88 |
|
0.00 |
| SD7043 |
|
9.07 |
| SD7043 (9.1%) |
|
9.10 |
| SD7062 |
|
13.92 |
| SD7062 (14%) |
|
14.00 |
| SD7080 |
|
9.05 |
| SD7080 (9.2%) |
|
9.20 |
| SD7084 |
|
9.61 |
| SD7084 (9.6%) |
|
9.60 |
| SD7090 |
|
9.97 |
| SD7090 (10%) |
|
10.00 |
| SD8000 |
|
8.84 |
| SD8000-089-88 |
|
0.00 |
| SD8020 |
|
10.10 |
| SD8020-010-88 |
|
0.00 |
| SD8040 |
|
9.89 |
| SD8040 (10%) |
|
10.00 |
| SELIG 3002-099-83 |
|
0.00 |
| SI-03010 |
|
10.00 |
| SIKORSKY DBLN-526 |
|
0.00 |
| SIKORSKY GS-1 |
|
0.00 |
| SIKORSKY SC1012R8 |
|
0.00 |
| SIKORSKY SC1094 R8 |
|
0.00 |
| SIKORSKY SC1094R8 |
|
0.00 |
| SIKORSKY SC1095 |
|
0.00 |
| SIKORSKY SC2110 |
|
0.00 |
| SIKORSKY SSC-A07 |
|
0.00 |
| SIKORSKY SSC-A09 |
|
0.00 |
| SMOOTHED ATR AIRFOIL |
airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program) |
0.00 |
| SOKOLOV |
|
0.00 |
| SPICA |
|
11.72 |
| SPICA 11.73% SMOOTHED |
|
11.73 |
| SSY |
|
12.50 |
| STRAND |
|
0.00 |
| TH 25816 HALE |
|
0.00 |
| TSAGI 12% |
|
12.00 |
| TSAGI 8% |
|
8.00 |
| UNIVERSITY OF ALBERTA UA 79-SF-187 |
|
0.00 |
| UNIVERSITY OF GLASGOW GU25-5(11)8 |
|
0.00 |
| UNIVERSITY OF ILLINOIS UI-1720 |
|
0.00 |
| USA 22 |
|
0.00 |
| USA 25 |
|
0.00 |
| USA 26 |
|
0.00 |
| USA 27 |
|
0.00 |
| USA 27 MOD. |
|
0.00 |
| USA 28 |
|
0.00 |
| USA 29 |
|
0.00 |
| USA 31 |
|
0.00 |
| USA 32 |
|
0.00 |
| USA 33 |
|
0.00 |
| USA 34 |
|
0.00 |
| USA 35 |
|
0.00 |
| USA 35 A |
|
0.00 |
| USA 40 |
|
0.00 |
| USA 40 B |
|
0.00 |
| USA 41 |
|
0.00 |
| USA 45 |
|
0.00 |
| USA 45 M |
|
0.00 |
| USA 46 |
|
0.00 |
| USA 48 |
|
0.00 |
| USA 49 |
|
0.00 |
| USA 5 |
|
0.00 |
| USA 50 |
|
0.00 |
| USA 51 |
|
0.00 |
| USA 98 |
|
0.00 |
| USA-27 |
|
11.04 |
| USA-35B |
|
0.00 |
| WASP (SMOOTHED) |
|
0.00 |
| WB-135/35 13.5% SMOOTHED |
|
13.50 |
| WB-140/35/FB 14% |
|
14.00 |
| WHITCOMB INTEGRAL SUPERCRITICAL |
|
0.00 |
| WORTMANN FX 049-915 |
|
0.00 |
| WORTMANN FX 05-188 |
|
0.00 |
| WORTMANN FX 05-191 |
|
0.00 |
| WORTMANN FX 05-H-126 |
|
0.00 |
| WORTMANN FX 057-816 |
|
0.00 |
| WORTMANN FX 08-S-176 |
|
0.00 |
| WORTMANN FX 082-512 |
|
0.00 |
| WORTMANN FX 2 |
|
0.00 |
| WORTMANN FX 3 |
|
0.00 |
| WORTMANN FX 60-126 |
Profil capable de supporter de fortes ChargesSupporte des cordes faibles (130m/m) Parfait pour cordes de 200 à 250 m/m Suppporte des virages serrés sans déclenchement. Pas moins de 40 gr/dm° pour 2.5m d'envergure (50 pour 3 m) |
|
| WORTMANN FX 60-126 G |
|
|
| WORTMANN FX 60-126-1 |
|
|
| WORTMANN FX 61-140 |
|
|
| WORTMANN FX 61-147 |
|
|
| WORTMANN FX 61-163 |
|
|
| WORTMANN FX 61-184 G |
|
|
| WORTMANN FX 62 K 131 |
|
|
| WORTMANN FX 62-K-131 |
|
0.00 |
| WORTMANN FX 62-K-131/17 |
|
|
| WORTMANN FX 62-K-153/20 |
|
|
| WORTMANN FX 63-137 |
Profil capable de supporter de fortes ChargesEncore plus porteur que le 60-126 A réserver aux cordes importantes |
|
| WORTMANN FX 63-143 |
|
|
| WORTMANN FX 63-147 |
|
|
| WORTMANN FX 66 S 161 |
|
|
| WORTMANN FX 66-17A-175 |
|
0.00 |
| WORTMANN FX 66-17AII-182 |
|
0.00 |
| WORTMANN FX 67 K 125/150 |
|
|
| WORTMANN FX 67 K 150 |
|
|
| WORTMANN FX 67-K-170 |
|
|
| WORTMANN FX 71 L 150 |
|
|
| WORTMANN FX 71-089A |
|
0.00 |
| WORTMANN FX 71-120 |
|
0.00 |
| WORTMANN FX 72 MS 150A |
|
|
| WORTMANN FX 72 MS 150B |
|
|
| WORTMANN FX 72-MS-150A |
|
0.00 |
| WORTMANN FX 72-MS-150B |
|
0.00 |
| WORTMANN FX 77-W-153 |
|
0.00 |
| WORTMANN FX 77-W-258 |
|
0.00 |
| WORTMANN FX 77-W-343 |
|
0.00 |
| WORTMANN FX 79-K-144/17 |
|
0.00 |
| WORTMANN FX L V-152 |
|
0.00 |
| WORTMANN FX LIII-142 |
|
|
| WORTMANN FX LV 152 K25 |
|
|
| WORTMANN FX M2 |
|
0.00 |
| WORTMANN FX S 02196 |
|
|