The Online Books Page

Books by James F. Schmidt:

Books in the extended shelves:

• Schmidt, James F.: Aerodynamic performances of three fan stator designs operating with rotor having tip speed of 337 meters per second and pressure ratio of 1.54 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Thomas F. Gelder, Genevieve M. Esgar, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust; US access only)
• Schmidt, James F.: Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) (National Aeronautics and Space Administration ;, 1974), also by Carroll A. Todd and Lewis Research Center (page images at HathiTrust)
• Schmidt, James F.: Experimental study of effect of simulated reactor core position on nozzle heat transfer (National Aeronautics and Space Administration ;, 1966), also by Lewis Research Center (page images at HathiTrust)
• Schmidt, James F.: Laminar skin-friction and heat-transfer parameters for a flat plate at hypersonic speeds in terms of free-stream flow properties (National Aeronautics and Space Administration, 1959), also by Lewis Research Center (page images at HathiTrust)
• Schmidt, James F.: NASA TN D-6595 (National Aeronautics and Space Administration :, 1972), also by Donald R. Boldman, Robert C. Ehlers, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Schmidt, James F.: Performance and boundary-layer evaluation of a sonic inlet (National Aeronautics and Space Administration ;, 1976), also by Robert S. Ruggeri and Lewis Research Center (page images at HathiTrust)
• Schmidt, James F.: Performance with and with inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Lewis Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Schmidt, James F.: Similar solutions for turbulent boundary layer with large favorble pressures gradients (nozzle flow with heat transfer) (National Aeronautics and Space Administration, 1971), also by Carroll Todd, Donald R. Boldman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Schmidt, James F.: Turbulence, heat-transfer, and boundary layer measurements in a conical nozzle with a controlled inlet velocity profile (National Aeronautics and Space Administration :, 1966), also by Donald R. Boldman, Anthony Fortini, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Schmidt, James F.: Turbulent skin-friction and heat-transfer coefficients for an inclined flat plate at high hypersonic speeds in terms of free-stream flow properties. (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)

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