Shock Tunnel Studies of Scramjet Phenomena 1994
Richard G. Morgan, A. Paull, R. J. Stalker
Abstract
Richard G. Morgan, A. Paull, R. J. Stalker
Abstract
Reports by the research staff and graduate students of the Mechanical Engineering Department at the University of Queensland are collected and presented. These reports cover various studies related to the advancement of scramjet technology and the operation of advanced hypervelocity shock-expansion tubes. The report topics include the experimental studies of mixing and combustion in a scramjet flow path, the measurement of integrated thrust and skin friction, and the development of a free-piston-driven expansion tunnel capable of delivering a test gas at superorbital velocities.
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Reports by the research staff and graduate students of the Mechanical Engineering Department at the University of Queensland are collected and presented. These reports cover various studies related to the advancement of scramjet technology and the operation of advanced hypervelocity shock-expansion tubes. The report topics include the experimental studies of mixing and combustion in a scramjet flow path, the measurement of integrated thrust and skin friction, and the development of a free-piston-driven expansion tunnel capable of delivering a test gas at superorbital velocities.
Key concepts: Expansion tunnel, Scramjet, Aerospace engineering, Shock (circulatory), Engineering, Hypersonic speed, Piston (optics), Mechanical engineering