Search results for: Burley, James R.
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1
Experimental and numerical results for a generic axisymmetric single-engine afterbody with horizontal and vertical tails at transonic speeds
Authors: Burley, James R.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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2
Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end
Authors: Burley, James R.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984Physical Description: 1 volume.Holdings: Loading…
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3
Investigation of installation effects on single-engine convergent-divergent nozzles
Authors: Burley, James R.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982Physical Description: 231 pages : illustrations ; 28 cm.Holdings: Loading…
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4
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
Authors: Burley, James R.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986Physical Description: 1 volume.Holdings: Loading…
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5
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
Authors: Mason, Mary L., Burley, James R.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986Physical Description: 1 online resource (54 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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6
Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display
Authors: Jones, Denise R., Abbott, Terence S., Burley, James R.
Published: NASA Langley Research Center, 1993Physical Description: 1 online resource (8 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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7
Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
Authors: Henderson, William P.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
Physical Description: 1 volume.Holdings: Loading…
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8
Qualitative evaluation of a conformal velocity vector display for use at high angles-of-attack in fighter aircraft
Authors: Jones, Denise R.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Langley Research Center, 1990
Physical Description: 1 volume.Holdings: Loading…
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9
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
Authors: Mason, Mary L.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986
Physical Description: 1 volume.Holdings: Loading…
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10
Performance characteristics of an isolated coannular plug nozzle at transonic speeds
Authors: Mercer, Charles E.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Available from the National Technical Information Service], 1985
Physical Description: 1 volume.Holdings: Loading…
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11
Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
Authors: Leavitt, Laurence D.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
Physical Description: 1 online resource (106 pages) : digital, PDF file.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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12
Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
Authors: Leavitt, Laurence D.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
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13
Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles
Authors: Carlson, John R.Other Authors:
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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14
Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle
Authors: Carson, George T.Other Authors:
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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15
Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
Authors: Pendergraft, Odis C.Other Authors: “…Burley, James R.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service [distributor], 1986
Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Jet nozzles
Static tests
Aerodynamics
Aerodynamics, Transonic
Nozzle geometry
Nozzles
Testing
Airplanes
Axisymmetric flow
Fighter planes
Motors
Nozzle thrust coefficients
Pitching (Aerodynamics)
Short take-off and landing aircraft
Thrust
Wind tunnel tests
Aerodynamic load
Aeronautical instruments
Afterburning
Air ducts
Annular nozzles
Attitude (inclination)
Boattails
Drag (Aerodynamics)
Flight simulation
Helmet mounted displays
High aspect ratio
Jet blast effects
Judgments
Mach number