The Online Books Page

Books by William J. Monta:

Books in the extended shelves:

• Monta, William J.: Description and calibration of the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charlie M. Jackson, William A. Corlett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Monta, William J.: Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 (National Aeronautics and Space Administration :, 1961), also by K. R. Czarnecki, Paul W. Howard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Monta, William J.: Effects of conventional and square stores on the longitudinal aerodynamic characteristics of a fighter aircraft model at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Monta, William J.: Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at mach 1.60 to 2.87 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by M. Leroy Spearman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Monta, William J.: Effects of stores on longitudinal aerodynamic characteristics of a fighter at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Samuel M. Dollyhigh, Giuliana Sangiogio, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Monta, William J.: Longitudinal aerodynamic characteristics at Mach 0.60 to 2.86 of a fighter configuration with strut braced wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Samuel M. Dollyhigh, Giuliana Sangiorgio, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Monta, William J.: NASA TN D-2048 (National Aeronautics and Space Administration, 1963), also by K. R. Czarnecki, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Monta, William J.: NASA TN D-3588 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by John B. Peterson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Monta, William J.: NASA TN D-4746 (National Aeronautics and Space Administration :, 1968), also by William D. Deveikis, K. R. Czarnecki, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Monta, William J.: Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by James M. Cubbage and Langley Research Center (page images at HathiTrust)
• Monta, William J.: Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration :, 1961), also by K. R. Czarnecki and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Monta, William J.: Supersonic aerodynamic characteristics of a Sparrow III type missile model with wing controls and comparison with existing tail-control results (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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