The Online Books Page

Books by Glenn A. Mitchell:

Books in the extended shelves:

• Mitchell, Glenn A.: Annular internal-external-expansion rocket nozzles for large booster applications (National Aeronautics and Space Administration :, 1961), also by James F. Connors, Robert W. Cubbison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mitchell, Glenn A.: Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Robert J. Shaw, Bobby W. Sanders, and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Robert J. Shaw, Bobby W. Sanders, and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbojet stall margin (National Aeronautics and Space Administration ;, 1975), also by Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Forward-slanted slot throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Robert J. Shaw, Bobby W. Sanders, and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 (National Aeronautics and Space Administration, 1960), also by Owen H. Davis and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 (National Aeronautics and Space Administration, 1960), also by John L. Allen, Owen H. Davis, and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Poppet valve control of throat stability bypass to increase stable airflow range of a Mach 2.5. inlet with 60 percent internal contraction (National Aeronautics and Space Administration ;, 1975), also by Bobby W. Sanders and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Pressure-activated stability-bypass-control valves to increase the stable airflow range of a Mach 2.5 inlet with 40 percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Bobby W. Sanders and Lewis Research Center (page images at HathiTrust)
• Mitchell, Glenn A.: Throat stability-bypass systems to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Robert J. Shaw, Bobby W. Sanders, and Lewis Research Center (page images at HathiTrust)

Find more by Glenn A. Mitchell at your library, or elsewhere.