Up to present turbojet engines employed have been essentially subsonic engines suitably strengthened; future may bring use of engines specifically designed for appropriate range of Mach number; some implications of this change of outlook reviewed in so far as they affect prediction of engine performance.
Some aspects of turbojet performance calculation at high flight Mach numbers
Aircraft Eng
Aircraft Engineering ; 28 , n 333
1956
5 pages
Aufsatz (Zeitschrift)
Englisch
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Some Aspects of Turbojet Performance Calculation at High Flight Mach Numbers
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