Modifications of the Shock Tube for the Generation of Hypersonic Flow

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Report Number: AEDC TN 55-15
Author(s): Hertzberg, A., Smith, W. E., Glick, H. S., Squire, W.
Corporate Author(s): Cornell Aeronautical Lab, Inc.
Date of Publication: 1955-03
Pages: 109
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PB Number: PB118115
Identifier: AD0056190

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