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INGC-MON-12436 |
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20221019004407.0 |
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060510s1964 |||a fr||||| |0 0|eng d |
| 080 |
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|a 531.3-255
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| 245 |
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|a Supersonic flow chemical processes and radiative transfer
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| 260 |
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|a New York :
|b Pergamon Press,
|c 1964.
|
| 300 |
|
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|a 488 p.
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| 505 |
0 |
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|a Mixing Problems with Chemical Reactions; Zakkay; Krause. V.. E.;Influence des Reactions Chimiques sur L'Ecoulement; Barrere. M.;Supersonic Diffusion Flames; Schetz. J. A.;Combustion supersonique dans un Canal Cylindrique; Mestre; Viaud. A.. L.;An investigation of Real Gas Effects Relevant to the Performance of Kerosine Fuelled Hypersonic Ramjet; Hawkins; Fox. R.. M. D.;Some effects of Stable Combustion in Wakes Formed in a Supersonic Stream; Townend; Reid. L. H.. J.;Chemical Relaxation for Channel Flows of Doubly Reacting Mixtures; Napolitano. L. G.;The Structure of the Rocket Exhaust Plume Without Reaction at Various Altitudes; Adamson, Jr.. T. C.;Transonic Aspects of Hypervelocity Rocket Plumes; Bowyer; D'Attore; Yoshihara. J.. L.. H.;The calculation od heat and mass transfer through the turbulent boundary layer on a flat plate at high mach numbers, with and without chemical reaction; Spalding; Auslander; Sundaram. D. B.. D. M.. T. R.;Similarity Parameters for Radiative Energy Transfer in Isothermal and Non-Isothermal Gas Mixtures; Penner; Thomas; Adomeit. S. S.. M.. G.;Radiation Transfer Regimes in Hypersonic Flight; Goulard. R.;Heat Transfer in Hypersonic Flow with Radiation and Chemical Reaction; Scala; Sampson. S. M.. D. H.;The Influence of Radiant-Energy Transfer on One-Dimensional Shock Ware Propagation; Olfe. D. B.;On Photoionization Ahead of a Strong Shock Ware; Ferrari; Clarke. C.. J. H.;Radiative Ionization Fronts in Hydrogen; Goldsworthy. F. A.;Laboratory Astrophysics and Combustion Spectroscopy; Nicholls. R. W.;Radiation Heat Transfer during Reentry; Kivel. B.;Thermal Radiation of a Flame with Condensed MgO Particles; Rössler. F.;Radiation Cooling of Aerodynamically Heated Surfaces at High Mach Numbers; Rosner. D. E.;Comments on Applicability of the Rosseland Approximation to Shock-heated Air; Penner. S. S.
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| 599 |
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|a Ubic.:533.2 OLF PRESA0339 Ubic.:533.2 OLF PRES
|
| 650 |
1 |
4 |
|a FLUJO SUPERSONICO
|9 274742
|
| 650 |
1 |
4 |
|a PROCESOS QUIMICOS
|9 263247
|
| 650 |
1 |
4 |
|a REACCIONES QUIMICAS DEL FLUJO
|9 292264
|
| 650 |
1 |
4 |
|a MEZCLA DE REACCIONES QUIMICAS
|9 292265
|
| 650 |
1 |
4 |
|a DIFUSION DE LLAMA SUPERSONICA
|9 292266
|
| 650 |
1 |
4 |
|a COMBUSTION SUPERSONICA
|9 292267
|
| 650 |
1 |
4 |
|a RAMJET
|9 285946
|
| 650 |
1 |
4 |
|a PERFORMANCE DE UN RAMJET
|9 292268
|
| 650 |
1 |
4 |
|a ONDAS DE EXPANSION
|9 286260
|
| 650 |
1 |
4 |
|a ONDAS DE COMPRESION
|9 285120
|
| 650 |
1 |
4 |
|a TERMODINAMICA
|9 262699
|
| 650 |
1 |
4 |
|a CHORRO DE GASES
|9 292269
|
| 650 |
1 |
4 |
|a FLUJO HIPERSONICO
|9 283696
|
| 650 |
1 |
4 |
|a PLACA PLANA
|9 285210
|
| 650 |
1 |
4 |
|a TRANSFERNCIA DEL CALOR
|9 292270
|
| 650 |
1 |
4 |
|a GAS IONIZADO
|9 292271
|
| 650 |
1 |
4 |
|a RADIACION TERMICA
|9 265263
|
| 650 |
1 |
4 |
|a CAPA LIMITE
|9 264004
|
| 700 |
0 |
|
|a Olfe, D. B.,
|e ed.
|9 292272
|
| 700 |
0 |
|
|a Zakkay, V.,
|e ed.
|9 292273
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
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|a MON
|
| 960 |
|
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|a 13193
|
| 970 |
|
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|a Registro convertido en forma automatizada
|
| 990 |
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|a GBY
|
| 999 |
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|c 12434
|d 12434
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| 040 |
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|a AR-LpUFI
|c AR-LpUFI
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