Books by Louis J. Goldman:
Books in the extended shelves:
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Goldman, Louis J.: Analytic investigation of effect of end-wall contouring on stator performance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert J. Boyle, Harold E. Rholik, and Lewis Research Center (page images at HathiTrust)- Goldman, Louis J.: Cold-air annular-cascade investigation of aerodynamic performance of cooled turbine vanes (National Aeronautics and Space Administration ;, 1974), also by Kerry L. McLallin and Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Cold-air annular-cascade investigation of aerodynamic performance of core-engine-cooled turbine vanes : II--Pressure surface trailing edge ejection and split trailing edge ejection (U.S. National Aeronautics and Space Administration ;, 1976), also by Kerry L. McLallin, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Design and operational performance of a 150-kilowatt sodium flash-vaporization facility Landon R. Nichols, Charles H. Winzig, Stanley M. Nosek and Louis J. Goldman. (National Aeronautics and Space Administration :, 1963), also by Landon R. Nichols, Stanley M. Nosek, Charles H. Winzig, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Goldman, Louis J.: Experimental nozzle expansion and flow characteristics of potassium vapor (National Aeronautics and Space Administration ;, 1966), also by Stanley M. Nosek and Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Laser anemometer measurements and computations in an annular cascade of high turning core turbine vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Richard G. Seasholtz and Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Laser anemometer measurements in an annular cascade of core turbine vanes and comparison with theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Richard G. Seasholtz, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Goldman, Louis J.: Prediction method for two-dimensional aerodynamic losses of cooled vanes using integral boundary-layer parameters (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Raymond E. Gaugler, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Three-component laser anemometer measurement systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Lewis Research Center (page images at HathiTrust)
- Goldman, Louis J.: Three component laser anemometer measurements in an annular cascade of core turbine vanes with contoured end wall (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Richard G. Seasholtz and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
- Goldman, Louis J.: Velocity surveys in a turbine stator annular-cascade facility using laser Doppler techniques (National Aeronautics and Space Administration ;, 1976), also by Kerry L. McLallin, Richard G. Seasholtz, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
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