The Online Books Page

Books by Bobby L. Berrier:

Books in the extended shelves:

• Berrier, Bobby L.: Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by E. Ann Bare, Francis J. Capone, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Berrier, Bobby L.: Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2 (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Berrier, Bobby L.: Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Francis J. Capone and Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Berrier, Bobby L.: Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by David E. Reubush and Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by John G. Taylor and Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Francis J. Capone, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Berrier, Bobby L.: Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Berrier, Bobby L.: Investigation of installation effects on single-engine convergent-divergent nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by James R. Burley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Berrier, Bobby L.: Investigation of installation effects on twin-engine convergent-divergent nozzles (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)
• Berrier, Bobby L.: NASA TN D-5655 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Charles E. Mercer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Berrier, Bobby L.: 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 Linda S. Bangert, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing (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)
• Berrier, Bobby L.: Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Mary L. Mason and Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Langley Research Center (page images at HathiTrust)
• Berrier, Bobby L.: Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Mary L. Mason and Langley Research Center (page images at HathiTrust)

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