Books by Theodore R. Creel:
Books in the extended shelves:
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Creel, Theodore R.: Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James L. Dillon and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)- Creel, Theodore R.: Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jim A. Penland, James L. Dillon, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Creel, Theodore R.: Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Fang-Jenq Chen, Ivan E. Beckwith, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Creel, Theodore R.: A device for rapid determination of thermophysical properties of phase-change wind-tunnel models (National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Creel, Theodore R.: Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by W. E. Zorumski, Ivan E. Beckwith, Barbara B. Holley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Creel, Theodore R.: Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
- Creel, Theodore R.: Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing (National Aeronautics and Space Administration ;, 1974), also by Jim A. Penland, Floyd G. Howard, and Langley Research Center (page images at HathiTrust)
- Creel, Theodore R.: NASA TN D-3541 (National Aeronautics and Space Administration :, 1966), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Creel, Theodore R.: Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Ivan E. Beckwith, J. Wayne Keyes, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Creel, Theodore R.: Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Fang-Jenq Chen, Ivan E. Beckwith, and Langley Research Center (page images at HathiTrust)
- Creel, Theodore R.: Pressure distributions and aerodynamic characteristics of 9⁰ and 15⁰ blunted cones in nitrogen and helium at Mach 20 (National Aeronautics and Space Administration, 1968) (page images at HathiTrust)
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