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Last edited by ImportBot
September 14, 2008 | History
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Richard J. Re

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8 works Add another?

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  • Cover of: Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

    First published in 1998 — 4 editions
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  • Cover of: Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration

    First published in 1979 — 2 editions
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  • Cover of: Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20

    First published in 1978 — 2 editions
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  • Cover of: Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports

    First published in 1987 — 1 edition
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  • Cover of: Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

    First published in 1986 — 1 edition
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  • Cover of: Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft

    First published in 1991 — 1 edition
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  • Cover of: Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92

    First published in 1993 — 1 edition
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  • Cover of: A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

    First published in 1996 — 1 edition
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We need a photo of Richard J. Re

Subjects

Jet nozzles, Jet planes, Mach number, Static pressure, Thrust reversers, Wind tunnel tests, Aerodynamics, Hypersonic, Aircraft engines, Airplanes, Angle of attack, Bodies of revolution, Bow waves, Canard Wings, Drag (Aerodynamics), Engine inlets, Hypersonic Aerodynamics, Nozzle geometry, Pressure distribution, Shock waves, Short take-off and landing aircraft, Static tests, Subsonic flow, Supersonic speed, Supersonic transports, Testing

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ID Numbers

  • OLID: OL4666515A

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History

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September 14, 2008 Created by ImportBot Imported from Oregon Libraries MARC record