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- W774425535 abstract "An assessment was made of the aerodynamic uncertainties associated with the design of a cold-deck-environment Navy VSTOL fighter/attack aircraft utilizing jet-diffuser ejectors for vertical lift and vectored-engine-over-wing blowing for supercirculation benefits. The critical aerodynamic uncertainties were determined as those associated with the constraints which size the aircraft to a specified set of requirements. A wind tunnel model and test programs are recommended for resolving these uncertainties." @default.
- W774425535 created "2016-06-24" @default.
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- W774425535 date "1978-05-01" @default.
- W774425535 modified "2023-09-27" @default.
- W774425535 title "Study of aerodynamic technology for VSTOL fighter/attack aircraft, volume 1" @default.
- W774425535 hasPublicationYear "1978" @default.
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