Justification and requirements are presented for a large subsonic wind tunnel capable of testing full scale aircraft, rotor systems, and advanced V/STOL propulsion systems. The design considerations and constraints for such a facility are reviewed, and the trades between facility test capability and costs are discussed.
The requirements for a new full scale subsonic wind tunnel
1972-02-01
Report
No indication
English
OPTIMUM FULL-SCALE SUBSONIC WIND TUNNEL
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