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Penland, Jim A. 1924-2010
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1416903
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Penland, Jim A.
Penland, Jim A. 1924-2010
Penland Jim A.
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Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90
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Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
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