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060510s1960 |||a fr||||| |0 0|fre d |
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|a 531.373.23
|
100 |
0 |
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|a George, L.
|9 286154
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245 |
0 |
0 |
|a La mécanique du vol :
|b Performances des avions et des engins
|
260 |
|
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|a Paris :
|b Librarie Polytechique,
|c 1960.
|
300 |
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|a p. 464
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599 |
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|a Ubic.:531.373.23 GEO PRES
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650 |
1 |
4 |
|a MECANICA DE VUELO
|9 271009
|
650 |
1 |
4 |
|a PERFORMANCE DE AVIONES
|9 283699
|
650 |
1 |
4 |
|a PERFORMANCE DE MOTORES
|9 286155
|
650 |
1 |
4 |
|a AERODINAMICA
|9 268671
|
650 |
1 |
4 |
|a MOTORES
|9 265156
|
650 |
1 |
4 |
|a TURBORREACTORES
|9 283818
|
650 |
1 |
4 |
|a TURBOHELICE
|9 286156
|
650 |
1 |
4 |
|a FUERZAS AERODINAMICAS
|9 281617
|
650 |
1 |
4 |
|a PERFILES AERODINAMICOS
|9 280267
|
650 |
1 |
4 |
|a PLANTA ALAR
|9 283984
|
650 |
1 |
4 |
|a VUELO TRANSONICO
|9 286157
|
650 |
1 |
4 |
|a VUELO SUPERSONICO
|9 283602
|
650 |
1 |
4 |
|a ATMOSFERA STANDAR
|9 281616
|
650 |
1 |
4 |
|a SUSTENTACION
|9 281871
|
650 |
1 |
4 |
|a PERFORMANCE
|9 281540
|
650 |
1 |
4 |
|a POTENCIA REQUERIDA
|9 285810
|
650 |
1 |
4 |
|a CARACTERISTICAS DE VUELO
|9 285254
|
650 |
1 |
4 |
|a VUELO CURVILINEO
|9 284488
|
650 |
1 |
4 |
|a PLANEO
|9 281979
|
650 |
1 |
4 |
|a VUELO EN ASCENSO
|9 285432
|
650 |
1 |
4 |
|a ATERRIZAJE
|9 281722
|
650 |
1 |
4 |
|a DESPEGUE
|9 281718
|
650 |
1 |
4 |
|a AUTONOMIA
|9 285942
|
650 |
1 |
4 |
|a AVIONES DE TRANSPORTE
|9 286158
|
650 |
1 |
4 |
|a VUELO EN MANIOBRA
|9 286159
|
650 |
1 |
4 |
|a ESTABILIDAD
|9 264856
|
700 |
0 |
|
|a Vernet, Jean-Francois.
|9 286160
|
942 |
|
|
|c LIB
|6 _
|
959 |
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|a MON
|
960 |
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|a 10961
|
970 |
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|a Registro convertido en forma automatizada
|
999 |
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|c 10252
|d 10252
|
040 |
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|a AR-LpUFI
|c AR-LpUFI
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