Books by Raymond S. Colladay:
Books in the extended shelves:
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Colladay, Raymond S. (Raymond Strong): Analysis and comparison of wall cooling schemes for advanced gas turbine applications (National Aeronautics and Space Administration, 1972), also by United States National Aeronautics and Space Administration and Lewis Research Center (page images at HathiTrust)- Colladay, Raymond S. (Raymond Strong): An analysis of the capabilities and limitations of turbine air cooling methods (National Aeronautics and Space Administration ;, 1970), also by Jack B. Esgar, Albert Kaufman, and Lewis Research Center (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): Computer program for obtaining thermodynamic and transport properties of air and products of combustion of ASTM-A-1 fuel and air (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Steven A. Hipensteele and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): NASA TN D-6405 (National Aeronautics and Space Administration:, 1971) (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): Similarity constraints in testing of cooled engine parts (National Aeronautics and Space Administration ;, 1974), also by Francis S. Stepka and Lewis Research Center (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): Streakline flow visualization of discrete hole film cooling with holes inclined 30 ̊to surface (U.S. National Aeronautics and Space Administration ;, 1976), also by Jan M. Lane, Louis M. Russell, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection (National Aeronautics and Space Administration ;, 1976), also by Louis M. Russell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Colladay, Raymond S. (Raymond Strong): Thermal feasibility of using methane or hydrogen fuel for direct cooling of a first-stage turbine stator (National Aeronautics and Space Administration :, 1970), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
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