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Proposed aeroelastic and flutter tests for the National Transonic Facility (1981)

Stevenson, J. R.

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Publication Date: 2011-08-18

Description: Tests that can exploit the capability of the NTF and the transonic cryogenic tunnel, or lead to improvements that could enhance testing in the NTF are discussed. Shock induced oscillation, supersonic single degree control surface flutter, and transonic flutter speed as a function of the Reynolds number are considered. Honeycombs versus screens to smooth the tunnel flow and a rapid tunnel dynamic pressure reducer are recommended to improve tunnel performance.

Keywords: AERODYNAMICS

Type: NASA. Langley Research Center High Reynolds Number Res. - 1980; p 153-161

Format: text

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