Problems in modeling the complex interacting flow fields in the transonic speed regime are reviewed. The limitations of wind tunnel test capabilities are identified, and options for resolving the deficiency are examined. The evolution of the National Transonic Facility, and the various needs for research investigations to be done there are discussed. The relative priorities that should be given within and across subdisciplines for guidance in planning for the most effective use of the facility are considered.
The transonic Reynolds number problem
1977-01-01
Conference paper
No indication
English
Transonic low-Reynolds number airfoils
AIAA | 1992
|Transonic low Reynolds number airfoils
AIAA | 1991
|Reynolds number scaling at transonic speeds
AIAA | 1998
|Reynolds Number Effects in Transonic Flow
NTIS | 1989
|Reynolds number effects in transonic flow
TIBKAT | 1988
|