Search results for: Burley, James R.

Showing 1 - 15 results of 15 Refine Results
  1. 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], 1986
    Physical Description: 1 volume : illustrations ; 28 cm.
    Government Document Microfilm Book
  2. 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], 1984
    Physical Description: 1 volume.
    Government Document Microfilm Book
  3. 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], 1982
    Physical Description: 231 pages : illustrations ; 28 cm.
    Government Document Book
  4. 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, 1986
    Physical Description: 1 volume.
    Government Document Microfilm Book
  5. 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, 1986
    Physical Description: 1 online resource (54 pages) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  6. 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, 1993
    Physical Description: 1 online resource (8 pages) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  7. 7

    Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds

    Authors: Henderson, William P.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  8. 8

    Qualitative evaluation of a conformal velocity vector display for use at high angles-of-attack in fighter aircraft

    Authors: Jones, Denise R.
    Published: National Aeronautics and Space Administration, Langley Research Center, 1990
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  9. 9

    Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

    Authors: Mason, Mary L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  10. 10

    Performance characteristics of an isolated coannular plug nozzle at transonic speeds

    Authors: Mercer, Charles E.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Available from the National Technical Information Service], 1985
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  11. 11

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

    Authors: Leavitt, Laurence D.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 online resource (106 pages) : digital, PDF file.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  12. 12

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

    Authors: Leavitt, Laurence D.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  13. 13

    Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles

    Authors: Carlson, John R.
    Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986
    Other Authors:
    Physical Description: 1 volume : illustrations ; 28 cm.
    Government Document Microfilm Book
  14. 14

    Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle

    Authors: Carson, George T.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987
    Other Authors:
    Physical Description: 1 volume.
    Government Document Microfilm Book
  15. 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.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service [distributor], 1986
    Other Authors: “…Burley, James R.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book