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Evaluation of flow properties behind 120 degree and 140 degree included angle cones and a viking 75 entry vehicle at mach numbers from 1.60 to 3.95

By: Brown, Clarence A.
Contributor(s): Campbell, James F.
Material type: materialTypeLabelBookPublisher: Washington, D.C. National Aeronautics and Space Administration 1973Description: 100p.Subject(s): Flow properties
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