The Online Books Page

Books by Harvard Lomax:

Books in the extended shelves:

• Lomax, Harvard: The Calculation of downwash behind supersonic wings with an application to triangular plan forms (National Advisory Committee for Aeronautics, 1948), also by Max A. Heaslet and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Chordwise and compressibility corrections to slender-wing theory (National Advisory Committee for Aeronautics, 1951), also by Loma Sluder and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Comparison of experimental and numerical results for the flow of a perfect gas about blunt-nosed bodies / Mamoru Inouye and Harvard Lomax. (National Aeronautics and Space Administration :, 1962), also by Mamoru Inouye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lomax, Harvard: Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations (National Advisory Committee for Aeronautics, 1949), also by Max A. Heaslet and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Linearized lifting-surface theory for swept-back wings with slender plan forms (National Advisory Committee for Aeronautics, 1949), also by Max A. Heaslet and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: NASA TN D-4109 (National Aeronautics and Space Administration ;, 1967), also by Harry E. Bailey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lomax, Harvard: NASA TN D-5176 (National Aeronautics and Space Administration ;, 1969), also by Franklyn B. Fuller, Harry E. Bailey, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lomax, Harvard: Numerical analysis of flow properties about blunt bodies moving at supersonic speeds in an equilibrium gas (National Aeronautics and Space Administration :, 1964), also by Mamoru Inouye, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lomax, Harvard: On the construction of highly stable, explicit, numerical methods for integrating coupled ordinary differential equations with parasitic eigenvalues (National Aeronautics and Space Administration ;, 1968), also by United States National Aeronautics and Space Administration and Ames Research Center (page images at HathiTrust)
• Lomax, Harvard: An operational unification of finite difference methods for the numerical integration of ordinary differential equations. (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1967) (page images at HathiTrust)
• Lomax, Harvard: Stable implicit and explicit numerical methods for integrating quasi-linear differential equations with parasitic-stiff and parasitic-saddle eigenvalues (National Aeronautics and Space Administration ;, 1968), also by United States National Aeronautics and Space Administration and Ames Research Center (page images at HathiTrust)
• Lomax, Harvard: Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts (National Advisory Committee for Aeronautics, 1950), also by Franklyn B. Fuller, Max A. Heaslet, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Three-dimensional unsteady lift problems in high-speed flight : the triangular wing (National Advisory Committee for Aeronautics, 1951), also by Franklyn B. Fuller, Max A. Heaslet, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: Variants and extensions of a fast direct numerical Cauchy-Riemann solver, with illustrative applications (Natural Aeronautics and Space Administration :, 1977), also by E. Dale Martin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lomax, Harvard: Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems (National Advisory Committee for Aeronautics, 1947), also by Max A. Heaslet, Arthur L. Jones, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lomax, Harvard: The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes (National Advisory Committee for Aeronautics, 1955), also by Ames Research Center (page images at HathiTrust)

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