Books by James R. Burley:
Books in the extended shelves:
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Burley, James R.: Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by George T. Carson, E. Ann Bare, and Langley Research Center (page images at HathiTrust)- Burley, James R.: Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by William P. Henderson and Langley Research Center (page images at HathiTrust)
- Burley, James R.: Investigation of installation effects on single-engine convergent-divergent nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Bobby L. Berrier and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Burley, James R.: Performance characteristics of an isolated coannular plug nozzle at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Charles E. Mercer and Langley Research Center (page images at HathiTrust)
- Burley, James R.: Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Laurence D. Leavitt and Langley Research Center (page images at HathiTrust)
- Burley, James R.: Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by John R. Carlson, Linda S. Bangert, and Langley Research Center (page images at HathiTrust)
- Burley, James R.: Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Mary L. Mason and Langley Research Center (page images at HathiTrust)
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