The Online Books Page

Boundary layer flow

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• The Upper-branch stability of compressible boundary layer flows ([Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]), by J. S. B. Gajjar, J. W. Cole, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Numerical investigation of an internal layer in turbulent flow over a curved hill / ([Cleveland, Ohio : NASA Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1989]), by S. W. Kim and Lewis Research Center (page images at HathiTrust)
• 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)
• Noise from interaction of flow with rigid surfaces : a review of current status of prediction techniques / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Richard E. Hayden, Langley Research Center, and Beranek Bolt (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by J. Schneider, J. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• A method for analyzing dynamic stall of helicopter rotor blades / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Peter Crimi, Barry L. Reeves, Langley Research Center, and Avco Corporation (page images at HathiTrust)
• An experimental investigation at a Mach number of 4.95 of flow in the vicinity of a 90 degree interior corner alined with the free-stream velocity / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by P. Calvin Stainback and Langley Research Center (page images at HathiTrust)
• Representation of the electric field of longitudinal waves in a plasma /, by P. J. Lindstrom, Robert J. Papa, and sponsor Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)

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