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Finite difference theory

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• Supersonic turbulent boundary-layer flows with mass injection through slots and/or porous walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Alvin L. Murray, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• A viscous/potential flow interaction analysis method for multi-element infinite swept wings. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust)
• Laminar or turbulent boundary-layer flows of perfect gases or reacting gas mixtures in chemical equilibrium / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by E. Clay Anderson, Clark H. Lewis, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Gerald B. Gilbert, Philip G. Hill, Ames Research Center, and Dynatech R/D Company (page images at HathiTrust)
• The flow induced by the coalescence of two initially stationary drops / (Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion Springfield, Va. : National Technical Information Service, distributor, 1994), by M. R. Nobari, Gretar Tryggvason, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Cross-sectional deformations of monocoque beams and their side effects on the natural vibration frequencies / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Robert G. Thomson, Edwin T. Kruszewski, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A method of setting up finite-difference schemes for prediction equations /, by Wang Chung-Hao and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions /, by Nelson R. Bauld, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Clemson University. Department of Mechanical Engineering (page images at HathiTrust)

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