More about Warner L. Stewart:
| | Books by Warner L. Stewart: Books in the extended shelves: Stewart, Warner L.: 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 Warren J. Whitney and United States National Aeronautics and Space Administration (page images at HathiTrust) Stewart, Warner L.: Effect of a reduction in stator solidity on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, R. Y. Wong, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Stewart, Warner L.: Effect of high rotor pressure-surface diffusion on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1955), also by James W. Miser, Daniel E. Monroe, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Stewart, Warner L.: Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5. [Part] I, , Velocity-diagram study (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Stewart, Warner L.: A method for determining turbine design characteristics for rocket turbodrive applications (National Advisory Committee for Aeronautics, 1958), also by Warren J. Whitney, David G. Evans, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
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