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Modifications of the Shock Tube for the Generation of Hypersonic Flow
Author(s): Hertzberg, A., Smith, W. E., Glick, H. S., Squire, W.Corporate Author(s): Cornell Aeronautical Lab, Inc.
Date of Publication: 1955-03
Report number: AEDC TN 55-15
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Real Gas Effects in a Hypersonic Shock Tunnel
Author(s): Squire, W., Hertzberg, A., Smith, W. E.Corporate Author(s): Cornell Aeronautical Lab, Inc.
Date of Publication: 1955-03
Report number: AEDC TN 55-14
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Flow Phenomena in Starting a Hypersonic Shock Tunnel
Author(s): Glick, H. S., Hertzberg, A., Smith, W. E.Corporate Author(s): Cornell Aeronautical Lab, Inc.
Date of Publication: 1955-03
Report number: AEDC TN 55-16
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