The Online Books Page

Books by Coleman duP. Donaldson:

Books in the extended shelves:

• Donaldson, Coleman duP.: An approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow (NACA, 1949), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Donaldson, Coleman duP.: Behavior of solutions of the Navier-Stokes equations for a complete class of three-dimensional viscous vortices (Princeton, New Jersey : Aeronautical Research Associates of Princeton, Inc., [1960], 1960), also by Roger D. Sullivan, Aeronautical Research Associates of Princeton, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Donaldson, Coleman duP.: The effect of surface perturbations on the pressure distributions about blunt two-dimensional bodies at high Mach numbers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Wallace D. Hayes, Roger D. Sullivan, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Donaldson, Coleman duP.: The effect of wall friction on the strength of shock waves in tubes and hydraulic jumps in channels (National Advisory Committee for Aeronautics, 1949), also by Roger D. Sullivan and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Donaldson, Coleman duP.: Examination of the solutions of the Navier-Stokes equations for a class of three-dimensional vortices. Part 1, Velocity distributions for steady motion (Washington, D.C. : United States Air Force, Office of Scientific Research, 1960., 1960), also by Roger D. Sullivan, Aeronautical Research Associates of Princeton, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Donaldson, Coleman duP.: Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds (NACA, 1952), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Donaldson, Coleman duP.: Hypersonic flow theories for predicting pressures on blunt two-dimensional and on conical shapes (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1964), also by Richard A. Scheuing, Roger D. Sullivan, Wallace D. Hayes, John W. Brook, Robert E. Melnik, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), Aeronautical Research Associates of Princeton, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Donaldson, Coleman duP.: Investigation of a simple device for preventing separation due to shock and boundary-layer interaction (National Advisory Committee for Aeronautics, 1950), also by Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Donaldson, Coleman duP.: Note on the importance of imperfect-gas effects and variation of heat capacities on the isentropic flow of gases (NACA, 1948), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Donaldson, Coleman duP.: Preliminary investigation of supersonic diffusers (Langley Memorial Aeronautical Laboratory, 1945), also by Arthur Kantrowitz, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Donaldson, Coleman duP.: Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers (National Advisory Committee for Aeronautics, 1952), also by Roy H. Lange and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

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