Assuming that thermodynamic cycle selected meets required thrust and specific fuel consumption, characteristics required of engine are light weight, easy maintainability, long overhaul life, and reliability; areodynamic considerations and effects of high temperatures on engine components; cooling of turbine buckets; afterburner temperature; exhaust nozzle design.
Turbojet-engine mechanical design for high mach number flight
Aero/Space Eng
Aero/Space Engineering ; 17 , n 9
1958
5 pages
Aufsatz (Zeitschrift)
Englisch
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