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Online Books by

North American Rockwell Corporation

Books from the extended shelves:

• North American Rockwell Corporation: Aerodynamic stability and control/wind tunnel data correlation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by G. R. Casteel and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Conceptual design study of a V/STOL lift fan commercial short haul transport (National Aeronautics and Space Administration ;, 1973), also by Ronald G. Knight, Jerome A. Prizlow, William V. Powell, and Ames Research Center (page images at HathiTrust)
• North American Rockwell Corporation: Development of a nozzle to improve the turning of supersonic Coanda jets (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Paul M. Bevilaqua, J.D. Lee, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Development of NDT methods for advanced metallic composite materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by George Martin, John F. Moore, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Docket No. 72-1715 (United States : United States Court of Appeals for the Seventh Circuit, 1973., 1973), also by Inc T. R. W. (page images at HathiTrust; US access only)
• North American Rockwell Corporation: The early detection of fatigue damage (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by John F. Moore, George Martin, Schillings Tsang, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Evaluations of methods to predict flutter of wings with external stores (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Sidney Siegel, Lowell V. Andrew, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Exploratory development of nondestructive testing techniques for diffusion bonded interfaces (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by George Martin, F. M. Coate, J. F. Moore, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Exploratory development of nondestructive testing techniques for diffusion-bonded interfaces (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1968., 1969), also by George Martin, John F. Moore, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Heat-transfer and flow-field tests of the North American Rockwell/ General Dynamics Convair space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by W. R. Martindale, L. L. Trimmer, R. K. Matthews, General Dynamics Corporation. Convair Division, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• North American Rockwell Corporation: Investigation of subsonic duct distortion (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by C. J. MacMiller and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Propulsion system integration and test program (steady state) (U) summary (U). Part I. Integration technique and test activities (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Robert H. Johnson, United Aircraft Corporation. Pratt & Whitney Aircraft Division, General Motors Corporation. Allison Division, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Propulsion system integration and test program (steady state) (U) summary (U). Part II. Vehicle analysis studies (U) (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Robert H. Johnson, General Motors Corporation. Allison Division, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Propulsion system integration and test program (steady state). Part III. Nozzle interaction drag tests (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by R. C. Westphal, R. H. Johnson, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Research and development of nondestructive testing techniques for composites (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by George Martin, John F. Moore, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Study of spaceborne multiprocessing. Phase I (National Aeronautics and Space Administration ;, 1970), also by Louis J. Koczela and Electronics Research Center (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Theoretical flow field calculations for project ram (National Aeronautics and Space Administration ;, 1969), also by H. Webb and Langley Research Center (page images at HathiTrust)
• North American Rockwell Corporation: Theoretical frequency response functions and power spectra of the XB-70 response to atmospheric turbulence (National Aeronautics and Space Administration, 1970), also by Thomas E. Stenton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• North American Rockwell Corporation: Unsteady aerodynamic pressures in transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by L. V. Andrew and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: Variable mesh methods for differential equations (National Aeronautics and Space Administration ;, 1968), also by R. Van Wyk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• North American Rockwell Corporation: XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz (National Aeronautics and Space Administration ;, 1970), also by Arnold W. Martin, Warren D. Beaulieu, and Flight Research Center (U.S.) (page images at HathiTrust)
• North American Rockwell Corporation: XB-70 structural mode control system design and performance analyses (National Aeronautics and Space Administration, 1970), also by John H. Wykes, Alva S. Mori, Louis U. Nardi, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)

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