Books by Warren J. Whitney:
Books in the extended shelves:
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Whitney, Warren J.: Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Thomas P. Moffitt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Whitney, Warren J.: Analytical investigation of performance of two-stage turbine over a range of ratios of specific heats from 1.2 to 1 2/3 Warren J. Whitney and Warner L. Stewart. (National Aeronautics and Space Administration :, 1962), also by Warner L. Stewart and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Whitney, Warren J.: Cold-air investigation of 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine : II, Performance of 2-, 3-, and 3 1/2-stage configurations (National Aeronautics and Space Administration ;, 1977), also by Frank P. Behning, Harold J. Schum, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Whitney, Warren J.: Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Lewis Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Whitney, Warren J.: Cold-air investigation of 4 1/2-stage turbine with stage loading factor of 4.66 and high specific work output : I, Overall performance (National Aeronautics and Space Administration ;, 1977), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Whitney, Warren J.: Cold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine (National Aeronautics and Space Administration ;, 1975), also by Frank P. Behning, Harold J. Schum, and Lewis Research Center (page images at HathiTrust)
- Whitney, Warren J.: Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Frank P. Behning, Thomas P. Moffitt, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Whitney, Warren J.: Investigation of transonic turbine designed for zero diffusion of suction-surface velocity (National Advisory Committee for Aeronautics, 1954), also by R. Y. Wong, Daniel E. Monroe, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Whitney, Warren J.: A method for determining turbine design characteristics for rocket turbodrive applications (National Advisory Committee for Aeronautics, 1958), also by Warner L. Stewart, David G. Evans, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
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