The Online Books Page

Online Books by

Raymond E. Mineck

Books from the extended shelves:

• Mineck, Raymond E.: Adaptive wall wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), also by Marie H. Tuttle and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), also by James L. Hassell, Carl E. Freeman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mineck, Raymond E.: Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by Carl E. Freeman, U.S. Army Air Mobility Research and Development Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mineck, Raymond E.: Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), also by Myles F. Schwendemann and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Airframe, wing, and tail aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by Carl E. Freeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mineck, Raymond E.: Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), also by Acquilla S. Hill and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by Arthur W. Carter and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mineck, Raymond E.: Flow visualization studies of blowing from the tip of a swept wing / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), also by Jeannette W. Smith, Dan H. Neuhart, and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989) (page images at HathiTrust)
• Mineck, Raymond E.: An improved computational procedure for determining helicopter rotor blade natural modes / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), also by William H. Weller, Langley Research Center, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Mineck, Raymond E.: Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by Richard J. Margason and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mineck, Raymond E.: Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Mineck, Raymond E.: Wind-tunnel investigation of a simulated gunship helicopter engine-exhaust-windstream interaction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by John C. Wilson and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Wind-tunnel investigation of helicopter-rotor wake effects on three helicopter fuselage models / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), also by John C. Wilson and Langley Research Center (page images at HathiTrust)
• Mineck, Raymond E.: Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes / (Washington, D.C. : National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ; [Springfield, Va. : Fo r sale by the National Technical Information Service], 1980), also by John D. Berry, Army Research and Technology Laboratories (U.S.). Structures Laboratory, United States. Army Aviation Research and Development Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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