The Online Books Page

Books by Laurence D. Leavitt:

Books in the extended shelves:

• Leavitt, Laurence D.: Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Linda S. Bangert, David E. Reubush, and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Jeffery A. Yetter, Langley Research Center, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Long P. Yip and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Leavitt, Laurence D.: Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by E. Ann Bare and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Bobby L. Berrier, Linda S. Bangert, and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45? (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by William P. Henderson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard J. Re, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles (National Aeronautics and Space Administation, Scientific and Technical Information Branch ;, 1984), also by Richard J. Re and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Linda S. Bangert and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: 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 James R. Burley and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Richard J. Re and Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Langley Research Center (page images at HathiTrust)
• Leavitt, Laurence D.: Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Richard J. Re and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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