More about Bruce G. Powers:
| | Books by Bruce G. Powers: Books in the extended shelves: Powers, Bruce G.: Analytical study of ride smoothing benefits of control system configurations optomized for pilot handling qualities (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Powers, Bruce G.: Flight investigation of the roll requirements for transport airplanes in the landing approach (National Aeronautics and Space Administration ;, 1972), also by Euclid C. Holleman, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust) Powers, Bruce G.: Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 (National Aeronautics and Space Administration, 1960), also by Jack Nugent and United States National Aeronautics and Space Administration (page images at HathiTrust) Powers, Bruce G.: Handling qualities of the XB-70 airplane in the landing approach. (National Aeronautics and Space Administration :, 1970), also by Donald T. Berry, Flight Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Powers, Bruce G.: NASA TN D-3370 (National Aeronautics and Space Administration :, 1966), also by Flight Research Center (U.S.) and United States National Aeronautics and Space Administration (page images at HathiTrust) Powers, Bruce G.: Phugoid characteristics of YF-12 airplane with variable-geometry inlets obtained in flight tests at a Mach number of 2.9 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Powers, Bruce G.: Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing (National Aeronautics and Space Administration ;, 1973), also by David A. Kier and Flight Research Center (U.S.) (page images at HathiTrust)
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