An improved potential gradient method to calculate airloads on oscillating supersonic interfering surfaces

Report (1981)

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Published Date

19-01-1981

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NLR MP 81001 U

Abstract

A description is given of a computationally inqjroved potential gradient method to calculate unsteady aerodynamic derivatives in supersonic flow. Results are presented and comparisons are made with results of existing methods and with experimental data for a fighter-type wing.

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