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How Requirements Influence the Lift/Cruise Fan Aircraft
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English
Abstract
Lift Fan Multimission V/STOL aircraft provide new capabilities which could revolutionize Naval and Marine aviation but the design concept as well as the design philosophy must be carefully selected. Since the propulsion system is the crux of any V/STOL aircraft this is of primary importance followed by secondary design considerations such as fuselage sizing to accommodate the multimission requirements.
Authors
Citation
Ames, L., "How Requirements Influence the Lift/Cruise Fan Aircraft," SAE Technical Paper 751101, 1975, https://doi.org/10.4271/751101.Also In
References
- McDonnell Aircraft Company Report MDC A3434 “Operational Aspects of the Model 260 in Various Military Missions,” October 1975
- Congressional Record Proceedings and Debates of the 94th Congress, First Session 1975 4797 4798
- McDonnell Aircraft Company Report MDC A1588 “A Full Scale Test of a New V/STOL Control System Energy Transfer Control (ETC),” 15 June 1972 “Phase II - Engine Out Operation,” April 1973
- NSIA ASWAC Committee, Aircraft Subcommittee Ad Hoc Study Report MDC A2791 “Impact of Detection Systems on ASW Aircraft Design (U)” 19 April 1974