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
1981-09-01
Conference paper
No indication
English
The National Transonic Facility
IEEE | 1986
|Design considerations of the national transonic facility
NTRS | 1976
|The National Transonic Facility
NTRS | 1986
|