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.
Aircraft design using the National Transonic Facility
01.09.1981
Aufsatz (Konferenz)
Keine Angabe
Englisch
The National Transonic Facility
IEEE | 1986
|The National Transonic Facility
NTRS | 1986
|Design considerations of the national transonic facility
NTRS | 1976
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