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Last edited by ImportBot
September 13, 2008 | History

M. Leroy Spearman

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  • Cover of: The aerodynamics of some guided projectiles

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  • Cover of: Longitudinal aerodynamic characteristics at Mach numbers from 1.60 to 2.86 for a spanmissile with three wing planforms

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  • Cover of: Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10 to 53 at Mach numbers from 2.30 to 4.62

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  • Cover of: A review of 50 years of aerodynamic research with NACA/NASA

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  • Cover of: Scientific and technical training in the Soviet Union

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  • Cover of: Some comparisons of US and USSR aircraft design developments

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  • Cover of: Aerodynamic characteristics of some lifting reentry concepts applicable to transatmospheric vehicle design studies

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  • Cover of: Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions

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  • Cover of: An experimental and theoretical study of the aerodynamic characteristics of some generic missles concepts at Mach numbers from 2 to 6.8

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  • Cover of: An overview of some monoplanar missile programs

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  • Cover of: The application of some lifting-body reentry concepts to missle design

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  • Cover of: Design trends for Army/Air Force airplanes in the United States

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  • Cover of: Effects of body shape on the aerodynamics of a body of revolution at Mach numbers from 1.6 to 4.6

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  • Cover of: Effects of external stores on the aerodynamic characteristics of a 60ê Delta-wing fighter model at Mach 1.60 to 2.87

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  • Cover of: Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds

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  • Cover of: The evolution of the high-speed civil transport

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  • Cover of: Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10 deg to 53 deg at Mach numbers from 2.30 to 4.62

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  • Cover of: Some aerodynamic discoveries and related NACA/NASA research programs following World War II

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  • Cover of: Some lessons learned with wind tunnels

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  • Cover of: Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰

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History

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September 13, 2008 Created by ImportBot Imported from Oregon Libraries MARC record