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- W1539771840 abstract "A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concept powered by a series flow tandem fan propulsion system. Forward and aft mounted fans have independent flow paths for V/STOL operation and series flow in high speed flight. Mission, combat and V/STOL performance is calculated. Detailed aerodynamic estimates are made and aerodynamic uncertainties associated with the configuration and estimation methods identified. A wind tunnel research program is developed to resolve principal uncertainties and establish a data base for the baseline configuration and parametric variations." @default.
- W1539771840 created "2016-06-24" @default.
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- W1539771840 date "1982-02-01" @default.
- W1539771840 modified "2023-09-25" @default.
- W1539771840 title "Study of aerodynamic technology for single-cruise engine V/STOL fighter/attack aircraft" @default.
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- W1539771840 hasPublicationYear "1982" @default.
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