Books by Don M. Santman:
Books in the extended shelves:
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Santman, Don M.: Experimental and analytical determination of integrated airframe nozzle performance. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972, 1972), also by Edsel R. Glasgow, S. J. Smyth, R. F. Smith, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)- Santman, Don M.: Experimental and analytical determination of integrated airframe nozzle performance. Volume II, Operating manual for twin-nozzle/aftbody drag and internal nozzle performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Edsel R. Glasgow, R. D. Grennan, R. A. Fox, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)
- Santman, Don M.: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Santman, Don M.: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume II, Wind tunnel data identification and presentation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, D. A. Tappeiner, T. E. Charbonneau, D. K. Hill, R. D. Grennan, R. A. Fox, D. A. Fox, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Santman, Don M.: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume IV, Operating manual for subsonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Santman, Don M.: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume V, Operating manual for supersonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Santman, Don M.: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume VI, Revised operating manual for twin nozzle/afterbody drag and nozzle internal performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Santman, Don M.: Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet (National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration, Ames Research Center, and Inc Ellco Engineering (page images at HathiTrust)
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