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- W773702313 abstract "The advantages of oblique wings have been the subject of numerous theoretical studies, wind tunnel tests, low speed flight models, and finally a low speed manned demonstrator, the AD-1. The specific objectives of the OWRA program are: (1) to establish the necessary technology base required to translate theoretical and experimental results into practical mission oriented designs; (2) to design, fabricate and flight test an oblique wing aircraft throughout a realistic flight envelope, and (3) to develop and validate design and analysis tools for asymmetric aircraft configurations. The preliminary design phase of the project is complete and has resulted in a wing configuration for which construction is ready to be initiated." @default.
- W773702313 created "2016-06-24" @default.
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- W773702313 date "1989-02-01" @default.
- W773702313 modified "2023-09-27" @default.
- W773702313 title "The oblique-wing research aircraft: A test bed for unsteady aerodynamic and aeroelastic research" @default.
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