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laurence d leavitt

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Flight testingEffects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristicsLaurence D. Leavitt

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

Laurence D. Leavitt · For sale by the National Technical Information Service]

103 sayfa · 1983

Fighter planes / Jet nozzles / Tail surfaces / Flight testing

Jet nozzlesPerformance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flapsLaurence D. Leavitt

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

Laurence D. Leavitt · For sale by the National Technical Information Service]

33 sayfa · 1982

Nozzles / Jet nozzles

Supersonic nozzlesLongitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Laurence D. Leavitt · For sale by the National Technical Information Service]

133 sayfa · 1979

Aerodynamics, Supersonic / Supersonic Aerodynamics / Supersonic nozzles

Fighter planesEffect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2Laurence D. Leavitt

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2

Laurence D. Leavitt · National Aeronautics and Space Administration, Scientific and Technical Information Branch

220 sayfa · 1983

Flight testing / Air-engines / Fighter planes

Thrust reversalStatic internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilitiesLaurence D. Leavitt

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

Laurence D. Leavitt · NASA

106 sayfa · 1985

Nozzle design / Vanes / Thrust reversal

Supersonic nozzlesEffects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt

Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Laurence D. Leavitt · for sale by the National Technical Information Service

74 sayfa · 1978

Aerodynamics, Supersonic / Supersonic Aerodynamics / Supersonic nozzles

TestingStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰Laurence D. Leavitt

Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰

Laurence D. Leavitt · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1985

Jet nozzles / Testing

TestingStatic internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzlesLaurence D. Leavitt

Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles

Laurence D. Leavitt · National Aeronautics and Space Administration, Scientific and Technical Information Branch

21 sayfa · 1982

Jet planes / Thrust reversers / Mathematical models / Testing