The Online Books Page

Two dimensional flow

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• Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow (National Aeronautics and Space Administration ;, 1974), by William D. Beasley, Robert J. McGhee, and Langley Research Center (page images at HathiTrust)
• Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps (National Aeronautics and Space Administration ;, 1974), by Gene J. Bingham, Kevin W. Noonan, and Langley Research Center (page images at HathiTrust)
• Two-dimensional cold air cascade study of a film cooled turbine stator blade. II, Experimental results of full film cooling tests (National Aeronautics and Space Administration ;, 1975), by Herman W. Purst and Lewis Research Center (page images at HathiTrust)
• A genuinely multi-dimensional upwind cell-vertex scheme for the Euler equations (National Aeronautics and Space Administration, Institute for Computational Mechanics in Propulsion, 1989), by Kenneth G. Powell, Bram van Leer, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Cross-spectral functions based on von Karman's spectral equation (National Aeronautics and Space Administration ;, 1972), by John C. Houbolt, Asim Sen, Langley Research Center, and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections (National Aeronautics and Space Administration ;, 1973), by Gerald B. Gilbert, Philip G. Hill, Ames Research Center, and Dynatech R/D Company (page images at HathiTrust)
• Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings (National Aeronautics and Space Administration, 1960), by E. Widmayer, S. A. Clevenston, W. T. Lauten, and Langley Research Center (page images at HathiTrust)
• Methods of calculating fundamental solutions of the wave equation, with tables (National Aeronautics and Space Administration, 1959), by William A. Mersman and Ames Research Center (page images at HathiTrust)
• Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer (National Aeronautics and Space Administration ;, 1969), by Larry L. Lynes, Gary D. Kuhn, Jack Norman Nielsen, Nielsen Engineering & Research, and Ames Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.