Some flow problems in air and space propulsion systems under development in German Federal Republic are considered; they include cascade flows, in which influence of Reynolds number, Mach number, axial pressure ratio turbulence and boundary constraint have been studied; flows with heat addition at subsonic and supersonic speeds are dealt with, including reaction-kinetic effects in ignition of fuel and in recombination processes in expanding jets; flow problems which arose in development of rocket test beds for third stage of ELD O rocket are described and, in particular, special rocket steam generators and flow problems associated with strong cooling of hot rocket gases.
Recent german contributions to research in thermogasdynamics of aerospace propulsion systems
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 70 , n 667
1966
17 pages
Article (Journal)
English
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