The Online Books Page

Separated flow

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• A realizable Reynolds stress algebraic equation model (National Aeronautics and Space Administration, 1993), by Tsan-Hsing Shih, John L. Lumley, Jiang Zhu, Lewis Research Center, and Japan) Symposium on Turbulence Shear Flows : (Ninth : 1993 : Kyoto (page images at HathiTrust)
• Use of a single turning vane to eliminate flow separation in a space-limited 90° intake elbow of an axial-flow compressor (National Aeronautics and Space Administration ;, 1965), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model (National Aeronautics and Space Administration ;, 1990), by S. W. Kim, Lewis Research Center. Institute for Computational Mechanics in Propulsion, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Separated flow over bodies of revolution using an unsteady discrete-vorticity cross wake. Part 2, Computer program description (National Aeronautics and Space Administration ;, 1974), by F. J. Marshall, F. D. Deffenbaugh, Langley Research Center, and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
• Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration (National Aeronautics and Space Administration ;, 1976), by Marjorie E. Manro, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Static longitudinal stability of a rocket vehicle having a rear-facing step ahead of the stabilizing fins (National Aeronautics and Space Administration, 1961), by Robert J. Keynton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 (National Aeronautics and Space Administration, 1960), by Dudley George McConnell and Lewis Research Center (page images at HathiTrust)
• Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unstructured grid method (National Aeronautics and Space Administration, Langley Research Center, 1995), by Dennis B. Finley and Langley Research Center (page images at HathiTrust)

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