Books by Loren W. Acker:
Books in the extended shelves:
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Acker, Loren W.: Accelerations in fighter-airplane crashes (National Advisory Committee for Aeronautics, 1957), also by Jacob C. Moser, Dugald O. Black, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)- Acker, Loren W.: Description and design of liquid-metal radiator and condenser test facility (National Aeronautics and Space Administration ;, 1967), also by Seymour Lieblein, Nick J. Sekas, and Lewis Research Center (page images at HathiTrust)
- Acker, Loren W.: Design and performance of a liquid-hydrogen, liquid-oxygen gas generator for driving a 1000-horsepower turbine (National Aeronautics and Space Administration :, 1962), also by Nick J. Sekas and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Acker, Loren W.: Experimental steady-state performance of a multitube, centrally finned, potassium condensing radiator (National Aeronautics and Space Administration ;, 1967), also by Orlando A. Gutierrez, Nick J. Sekas, and Lewis Research Center (page images at HathiTrust)
- Acker, Loren W.: Inlet noise suppressor performance with a turbojet engine as the noise source (National Aeronautics and Space Administration, 1971), also by John F. Groeneweg, Charles E. Feiler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Acker, Loren W.: NASA TN D-4020 (National Aeronautics and Space Administration ;, 1967), also by David B. Fenn, Harold H. Coe, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Acker, Loren W.: NASA TN D-6178 (National Aeronautics and Space Administration ;, 1971), also by Edward J. Rice, Charles E. Feiler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Acker, Loren W.: Natural icing of an axial-flow turboject engine in flight for a single icing condition (National Advisory Committee for Aeronautics, 1948), also by Flight Propulsion Research Laboratory (page images at HathiTrust)
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