Results of simple performance calculations are given for turbojet and ramjet engines; influence of Mach number, compressor pressure ratio and turbine (combustion) temperature; characteristics of supersonic intakes with external and internal compression, matching of intake and engine, definitions of thrust and drag, additive drag and use of convergent-divergent tailpipes are discussed. (See also - n 6 Feb 9 1962 p L13-20)
Propulsion of supersonic airplanes
De voortstuwing van supersone vliegtuigen
Ingenieur ; 74 , n 9
1962
Article (Journal)
Dutch
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Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes
SAE Technical Papers | 1990
|Engineering Index Backfile | 1923
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