Separate development of intake and nozzle may lead to components which are individually very efficient; when integrated into unit some of efficiency may be lost in producing compatibility with engine and remainder of powerplant; it is often found that the most efficient components lack flexibility in face of changing atmospheric conditions; flexibility can be achieved by suitable development and choice of components which would reduce demands on intake control system without incurring severe penalty in performance; problem is treated in terms of quasi-static effects of changes in ambient temperature on performance.
Fully integrated propulsion system for supersonic transport aircraft
AGARDograph
1965
26 pages
Aufsatz (Zeitschrift)
Englisch
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