Gas turbine requirements for V/STOL aircraft are strongly influenced by type of airplane and mission to be performed; gas turbine requirements are established in several propulsion-system concepts which encompass majority of engine requirements necessary to V/STOL airplanes; specific requirements for air superiority fighter airplane, subsonic fighter attack airplane, and transport-cargo type of airplane are discussed; these three types of airplanes use propulsion systems incorporating lift turbojet engines, turbofan engines, fans with remote gas generators, and turboprop engines.
V/STOL aircraft gas turbine requirements
ASME -- Paper
ASME Meeting GT-48 ; 1967
1967
12 pages
Conference paper
English
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