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20221019003944.0 |
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060510s1984 |||a fr||||| |0 0|eng d |
| 080 |
|
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|a 629.735.4
|
| 245 |
0 |
0 |
|a Rotary-Wing Aerodynamics
|
| 260 |
|
|
|a New York :
|b Dover Publications,
|c 1984.
|
| 300 |
|
|
|a p. 236
|
| 599 |
|
|
|a Tomo:I Y II Ubic.:629.735.4 STE PRES
|
| 650 |
1 |
4 |
|a HELICOPTEROS
|9 283656
|
| 650 |
1 |
4 |
|a AERODINAMICA
|9 268671
|
| 650 |
1 |
4 |
|a ROTOR
|9 283837
|
| 650 |
1 |
4 |
|a ESTABILIDAD
|9 264856
|
| 650 |
1 |
4 |
|a CONTROL
|9 263886
|
| 650 |
1 |
4 |
|a HELICES
|9 274680
|
| 650 |
1 |
4 |
|a PALA
|9 284684
|
| 650 |
1 |
4 |
|a VORTICES
|9 285169
|
| 650 |
1 |
4 |
|a TEORIA DE VORTICES
|9 285809
|
| 650 |
1 |
4 |
|a TEORIA POTENCIAL
|9 283956
|
| 650 |
1 |
4 |
|a FLUJO POTENCIAL
|9 274608
|
| 650 |
1 |
4 |
|a PERFILES PARA ROTORES
|9 285960
|
| 650 |
1 |
4 |
|a PERFORMANCE
|9 281540
|
| 650 |
1 |
4 |
|a PERFORMANCE EN ASCENSO
|9 285961
|
| 650 |
1 |
4 |
|a RESISTENCIA
|9 265545
|
| 650 |
1 |
4 |
|a POTENCIA REQUERIDA
|9 285810
|
| 650 |
1 |
4 |
|a HELICOPTEROS CON ALAS
|9 285962
|
| 650 |
1 |
4 |
|a PERFORMANCE EN VUELO
|9 285963
|
| 650 |
1 |
4 |
|a VUELO ESTACIONARIO
|9 285964
|
| 650 |
1 |
4 |
|a DISCO ACTUADOR
|9 285807
|
| 650 |
1 |
4 |
|a HELICOPTEROS EN TANDEM
|9 285965
|
| 700 |
0 |
|
|a Keys, C. N.
|9 285966
|
| 700 |
0 |
|
|a Stepniewski, W. Z,
|e ed.
|9 285967
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
|
|a MON
|
| 960 |
|
|
|a 10903
|
| 970 |
|
|
|a Registro convertido en forma automatizada
|
| 990 |
|
|
|a SV
|
| 999 |
|
|
|c 10199
|d 10199
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| 040 |
|
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|a AR-LpUFI
|c AR-LpUFI
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