The requirements for a new full scale subsonic wind tunnel

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...

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Bibliographische Detailangaben
Hauptverfasser: Kelly, M. W., Mckinney, M. O., Luidens, R. W.
Format: Report
Sprache:eng
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Beschreibung
Zusammenfassung: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.