Books by Don E. Avery:
Books in the extended shelves:
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Avery, Don E.: Aerodynamic heating in gaps of thermal protection system tile arrays in laminar and turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978) (page images at HathiTrust)- Avery, Don E.: Aerodynamic heating on the corrugated surface of a 10.2⁰ half-angle blunted cone at Mach 6.7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Irving Weinstein, L. Roane Hunt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Avery, Don E.: Aerodynamic heating to the gaps and surfaces of simulated reusable-surface-insulation tile arrays in turbulent flow at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), also by Irving Weinstein, Andrew J. Chapman, and Langley Research Center (page images at HathiTrust)
- Avery, Don E.: Aerothermal performance and damage tolerance of a René 41 metallic standoff thermal protection system at mach 6.7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Avery, Don E.: Coastal currents and sewage disposal in the Hawaiian Islands ([Honolulu], 1964), also by Taivo Laevastu, Hawaii Dept. of Planning and Economic Development Hawaii's shoreline, and Doak C. Cox (page images at HathiTrust)
- Avery, Don E.: Electroless-plating technique for fabricating thin-wall convective heat-transfer models (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Maywood L. Wilson, Gary K. Ballard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Avery, Don E.: Experimental aerodynamic heating of simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Langley Research Center (page images at HathiTrust)
- Avery, Don E.: Performance of a Haynes 188 metallic standoff thermal protection system at Mach 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Avery, Don E.: Thermal and aerothermal performance of titanium multiwall thermal protection system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John L. Shideler, Lyndon B. Johnson Space Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
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