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Last edited by ImportBot
September 16, 2008 | History

Robert L Stallings

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  • Cover of: Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86

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  • Cover of: Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55ê swept delta wing at supersonic speeds

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  • Cover of: Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

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  • Cover of: Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds

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