The key features of the integrated propulsion systems developed for short haul aircraft are discussed including the high Mach number, fixed geometry, near sonic inlet, the variable area nozzles, thrust reversing systems, and aircraft accessory location. The roles and interplay of each element are considered and comparisons are made with conventional state-of-the-art technology.
Inlet/nacelle/exhaust system integration for the QCSEE propulsion systems
1976-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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