Books by John H. Crews:
Books in the extended shelves:
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Crews, John H.: Analytical and experimental investigation of fatigue in a sheet specimen with an interference-fit bolt (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)- Crews, John H.: The application of acoustic emission technique to fatigue crack measurement (National Aeronautics and Space Administration ;, 1974), also by Jag J. Singh, William T. Davis, and Langley Research Center (page images at HathiTrust)
- Crews, John H.: Cyclic debonding of unidirectional composite bonded to aluminum sheet for constant-amplitiude loading (National Aeronautics and Space Administration ;, 1976), also by George L. Roderick, Richard A. Everett, and Langley Research Center (page images at HathiTrust)
- Crews, John H.: An elastoplastic analysis of a uniaxially loaded sheet with an interference-fit bolt (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
- Crews, John H.: Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system (U.S. National Aeronautics and Space Administration ;, 1976), also by J. A. Sova, R. J. Exton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Crews, John H.: A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle (National Aeronautics and Space Administration ;, 1974), also by J. A. Sova and Langley Research Center (page images at HathiTrust)
- Crews, John H.: NASA TN D-3152 (National Aeronautics and Space Administration :, 1965), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Crews, John H.: Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Gregory R. Wichorek and Langley Research Center (page images at HathiTrust)
- Crews, John H.: Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading (National Aeronautics and Space Administration, Scientifice and Technical Information Office, 1979), also by C. S. Hong, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Crews, John H.: Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), also by I. S. Raju, C. S. Hong, Joint Institute for Advancement of Flight Sciences, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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