Problem of applying propulsion system to supersonic aircrafts; it is shown that neither turbojets nor ramjets are entirely satisfactory when used by themselves; satisfactory results of combining two power plants into propulsion system; comparison of performance along operating altitude Mach number paths in terms of thrust and specific fuel consumption only. (see also abstract in Soc Automotive Engrs -- J v 65 n 8 July 1957 p 35-8)
Ramjet-Turbojet propulsion system for supersonic flight
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957
1957
8 pages
Aufsatz (Konferenz)
Englisch
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Ramjet-Turbojet propulsion system for supersonic flight
Engineering Index Backfile | 1957
|THE RAMJET-TURBOJET PROPULSION SYSTEM FOR SUPERSONIC FLIGHT
SAE Technical Papers | 1957
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