Imagen de cubierta local
Imagen de cubierta local

Scramjet propulsion , Curran. E. T.

Colaborador(es): Tipo de material: PartituraPartituraSeries Progress in astronautics and aeronautics ; 189 | Zarchan, Paul ; Detalles de publicación: Reston American Institute of Aeronautics and AstronauticsDescripción: xxvii, 1293 p. gráficosISBN:
  • 1563473224
Contenidos:
Scramjet testing in the T3 and T4 hypersonic impulse facilities
Cramjet developments in France
Scramjet investigations within the german Hypersonics Technology Program (19931996)
Scramjet engine research at the National Space Laboratory in Japan
Scramjet research and development in Russia
Scramjet performance
Cramjet inlets
Supersonic flow combustors
Aerothermodynamics of the dualmode combustion system
Basic performance assessment of scram combustors
Strutjet rocketbased combinedcycle engine
Liquid hydrocarbon fuels for hypersonic propulsion
Detonationwawe ramjets
Problem of hypersonic flow deceleration by magnetic field
Rudiments an methodology for design and analysis of hypersonic airbreathing vehicles
Transatmospheric launcher sizing
Scramjet flowpath integration
Etiquetas de esta biblioteca: No hay etiquetas de esta biblioteca para este título. Ingresar para agregar etiquetas.
Valoración
    Valoración media: 0.0 (0 votos)
Existencias
Tipo de ítem Biblioteca actual Signatura topográfica Estado Fecha de vencimiento Código de barras
Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73./.78(036=111 SCR (Navegar estantería(Abre debajo)) Disponible 005862

Resúmenes, referencias bibliográficas, lecturas recomendadas y apéndices, al final de cada capítulo

Scramjet testing in the T3 and T4 hypersonic impulse facilities

Cramjet developments in France

Scramjet investigations within the german Hypersonics Technology Program (19931996)

Scramjet engine research at the National Space Laboratory in Japan

Scramjet research and development in Russia

Scramjet performance

Cramjet inlets

Supersonic flow combustors

Aerothermodynamics of the dualmode combustion system

Basic performance assessment of scram combustors

Strutjet rocketbased combinedcycle engine

Liquid hydrocarbon fuels for hypersonic propulsion

Detonationwawe ramjets

Problem of hypersonic flow deceleration by magnetic field

Rudiments an methodology for design and analysis of hypersonic airbreathing vehicles

Transatmospheric launcher sizing

Scramjet flowpath integration

No hay comentarios en este titulo.

para colocar un comentario.

Haga clic en una imagen para verla en el visor de imágenes

Imagen de cubierta local