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Last edited by ImportBot
September 16, 2008 | History

Jim A Penland

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  • Cover of: Low-speed aerodynamic characteristics of a lifting-body hypersonic research aircraft configuration

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  • Cover of: Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels

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  • Cover of: Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach number 0.2

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  • Cover of: Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0

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September 16, 2008 Created by ImportBot Imported from Miami University of Ohio MARC record