A novel efficient drive system has been developed which provides for the continuous operation of a pitot Mach 2.5 wind tunnel at compression ratios down to 0.625:1. The drive system does not require an overpressure to start, and no hysteresis has been observed. The general design of the proof-of-concept wind tunnel using the new drive system and its modifications are described.
An efficient supersonic wind tunnel drive system for Mach 2.5 flows
AIAA Applied Aerodynamics Conference
01.01.1991
Aufsatz (Konferenz)
Keine Angabe
Englisch
An Efficient Supersonic Wind Tunnel Drive System for Mach 2.5 Flows
British Library Conference Proceedings | 1991
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