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Aircraft design using the National Transonic Facility (1981)

Bonner, E.

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Publication Date: 2011-08-18

Description: The utility of the cryogenic high Reynolds number test facility as a production tunnel is evaluated. Aerodynamic performance evaluation, numerical wing design verification, and high Reynolds number theoretical extensions are considered. A priority ranking of NTF uses from an airframe development viewpoint is presented.

Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE

Type: NASA. Langley Research Center High Reynolds Number Res. - 1980; p 149-152

Format: text

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