Showing 1 - 4 results of 4 for search 'Re, Richard J.', query time: 0.01s
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Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / by Berrier, Bobby L., Re, Richard J.
Published 1980Call Number: Loading…CONNECT
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2
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / by Re, Richard J., Abeyounis, William Kelly
Published 1996Call Number: Loading…CONNECT
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Government Document Electronic eBook -
3
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel / by Re, Richard J., Capone, Francis J.
Published 1998Call Number: Loading…CONNECT
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Government Document Electronic eBook -
4
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / by Re, Richard J., Leavitt, Laurence D.
Published 1986Call Number: Loading…CONNECT
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Related Subjects
Mach number
Static pressure
Wind tunnel tests
Aircraft engines
Angle of attack
Bodies of revolution
Bow waves
Convergent-divergent nozzles
Engine inlets
Jet nozzles
Jet planes
Nozzle design
Nozzle geometry
Performance tests
Pressure distribution
Pressure ratio
Shock waves
Static tests
Subsonic flow
Supersonic speed
Supersonic transports
Thrust reversal
Thrust reversers
Thrust vector control