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| LEADER |
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| 001 |
INGC-MON-10105 |
| 003 |
AR-LpUFI |
| 005 |
20221019003933.0 |
| 008 |
060510s1962 |||a fr||||| |0 0|eng d |
| 080 |
|
|
|a 629.76
|
| 100 |
0 |
|
|a Dorrange, William H.
|9 285358
|
| 245 |
0 |
0 |
|a Viscous Hypersonic Flow :
|b Theory of Reacting and Hypersonic Boundary Layers
|
| 260 |
|
|
|a New York :
|b McGraw-Hill,
|c 1962.
|
| 300 |
|
|
|a 334 p.
|
| 440 |
0 |
0 |
|a M
|9 266295
|
| 599 |
|
|
|a Ubic.:629.76 MCG PRES
|
| 650 |
1 |
4 |
|a TURBULENCIA
|9 264020
|
| 650 |
1 |
4 |
|a CAPA LIMITE
|9 264004
|
| 650 |
1 |
4 |
|a CAPA LIMITE TURBULENTA
|9 274614
|
| 650 |
1 |
4 |
|a FLUJO TURBULENTO
|9 264022
|
| 650 |
1 |
4 |
|a FLUJO HIPERSONICO
|9 283696
|
| 650 |
1 |
4 |
|a TRANSFERENCIA DE CALOR
|9 263102
|
| 650 |
1 |
4 |
|a CAPA LIMITE LAMINAR
|9 274611
|
| 650 |
1 |
4 |
|a EFECTP DE CURVATURA
|9 285359
|
| 650 |
1 |
4 |
|a GRANDIENTE DE PRESION
|9 285360
|
| 650 |
1 |
4 |
|a TRANSFERENCIA DE MASA
|9 263084
|
| 650 |
1 |
4 |
|a ONDAS DE CHOQUE
|9 283779
|
| 650 |
1 |
4 |
|a VORTICIDAD
|9 282477
|
| 650 |
1 |
4 |
|a DISOCIADA LAMINAR
|9 285361
|
| 650 |
1 |
4 |
|a DISOCIADA TURBULENTA
|9 285362
|
| 650 |
1 |
4 |
|a REACCIONES QUIMICAS
|9 263234
|
| 650 |
1 |
4 |
|a MEZCLAS GASEOSAS
|9 285363
|
| 650 |
1 |
4 |
|a VISCOSIDAD
|9 266676
|
| 650 |
1 |
4 |
|a MISILES
|9 270214
|
| 650 |
1 |
4 |
|a TECNOLOGIA ESPACIAL
|9 285364
|
| 700 |
0 |
|
|a Guyford Stever, H.,
|e ed.
|9 285365
|
| 700 |
0 |
|
|a Seifert, Howard S.,
|e ed.
|9 285366
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
|
|a MON
|
| 960 |
|
|
|a 10801
|
| 970 |
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|
|a Registro convertido en forma automatizada
|
| 990 |
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|a SV
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| 999 |
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|c 10103
|d 10103
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| 040 |
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