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- W2317263552 abstract "The aerodynamic prediction methodology available in ACSYNT is examined through comparison with aircraft data for a variety of classes of configurations. The predictions are a synthesis of the best empirical procedures currently available. The paper presents selected results obtained from the comparison, and shows how the basic capability can be enhanced by user supplied adjustments to represent changes in technology levels when considering advanced aircraft designs. The predictions and basis for adjustments are described for a supersonic cruise vehicle (the xB-70), a large subsonic transport, and a typical fighter." @default.
- W2317263552 created "2016-06-24" @default.
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- W2317263552 date "1993-02-16" @default.
- W2317263552 modified "2023-09-23" @default.
- W2317263552 title "ACSYNT aerodynamic estimation - An examination and validation for use in conceptual design" @default.
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- W2317263552 doi "https://doi.org/10.2514/6.1993-973" @default.
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