A Pressure Control System for a Hypersonic Wind Tunnel
By W. H. Horton, I. L. Smith, Stanford University. Department of Aeronautics and Astronautics
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Contents: Introduction; Test Facility, Details of the Air Storage System; Regenerative Gas Fired Heat Exchanger; Air Flow Control System; Air Control Valves; Hydraulic System; Servo Amplifier; Pressure Sensing Devices; Control Computer-Design considerations, Construction details, Modus operandi of the analogue control; Resume of Performance.
Book Details
- Country: US
- Published: 1963
- Publisher: Department of Aeronautics and Astronautics, Stanford University
- Language: English
- Pages: 48
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