The Online Books Page

Books by M. Leroy Spearman:

Books in the extended shelves:

• Spearman, M. Leroy: Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spearman, M. Leroy: Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 (National Aeronautics and Space Administration ;, 1972), also by Ida K. Collins and Langley Research Center (page images at HathiTrust)
• Spearman, M. Leroy: Design trends for Army/Air Force airplanes in the United States (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Langley Research Center (page images at HathiTrust)
• Spearman, M. Leroy: 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 William J. Monta and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Spearman, M. Leroy: Effects of forebody length on the stability and control characteristics at a Mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing (National Aeronautics and Space Administration :, 1962), also by Cornelius Driver and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spearman, M. Leroy: Investigation of the aerodynamic characteristics in pitch and sideslip of a 45° swept-wing airplane configuration with various vertical locations of the wing and horizontal tail. Static lateral and directional stability ; Mach numbers of 1.41 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by Ross B. Robinson, United States. National Adviosry Committee for Aeronautics, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Spearman, M. Leroy: Longitudinal aerodynamic characteristics at Mach Numbers from 1.60 to 2.86 for a spanmissile with three wing planforms (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Wallace C. Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Spearman, M. Leroy: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Spearman, M. Leroy: Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 (National Advisory Committee for Aeronautics, 1959), also by Arthur Henderson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Spearman, M. Leroy: Stability and control characteristics at a mach number of 1.89 of a lightweight glider reentry configuration (National Aeronautics and Space Administration, 1960), also by Ross B. Robinson and Langley Research Center (page images at HathiTrust)
• Spearman, M. Leroy: Stability and control characteristics at a mach number of 2.01 of a supersonic VTOL airplane model having a broad fuselage and small delta wings (National Aeronautics and Space Administration, 1961), also by Cornelius Driver and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Spearman, M. Leroy: Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° (National Aeronautics and Space Administration, 1959), also by Gerald V. Foster, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Spearman, M. Leroy: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), also by Gerald V. Foster and Langley Research Center (page images at HathiTrust)
• Spearman, M. Leroy: Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 (National Aeronautics and Space Administration, 1959), also by Cornelius Driver and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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