NASA NTRS · 19810022601
Aircraft design using the National Transonic Facility
Abstract
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.
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Bonner, E.. 1981-09-01. Aircraft design using the National Transonic Facility. https://ntrs.nasa.gov/citations/19810022601
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