The Online Books Page

Books by Barrett L. Shrout:

Books in the extended shelves:

• Shrout, Barrett L.: Aerodynamic characteristics at Mach numbers from 0.6 to 2.16 of supersonic cruise fighter configuration with a design Mach mumber of 1.8 (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Shrout, Barrett L.: Aerodynamic characteristics of a series of bodies with variations in nose camber (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Peter F. Covell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Shrout, Barrett L.: Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Roger H. Fournier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Informaton Office (page images at HathiTrust)
• Shrout, Barrett L.: Effect of a simulated engine jet blowing above an arrow wing at mach 2.0 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Clyde Hayes and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Shrout, Barrett L.: Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by A. Warner Robins, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Shrout, Barrett L.: Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Ida K. Collins, William A. Corlett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

Find more by Barrett L. Shrout at your library, or elsewhere.