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Aerodynamic loads

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• Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 1, Model and results (National Aeronautics and Space Administration ;, 1971), by S. G. Sadler, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 2, Program listings (National Aeronautics and Space Administration ;, 1971), by S. G. Sadler, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume II, Aerodynamics and aerodynamic loads (National Aeronautics and Space Administration ;, 1970), by James C. Williams, John N. Perkins, Delbert C. Summey, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Supersonic flutter of a thermally stressed flat plate with edge stiffeners (National Aeronautics and Space Administration ;, 1970), by Harmohan Singh Singh, Charles Libove, Electronics Research Center (U.S.), and Syracuse University (page images at HathiTrust)
• Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 (National Aeronautics and Space Administration, 1961), by Marlowe D. Cassetti, William B. Igoe, Richard J. Re, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 (National Aeronautics and Space Administration, 1959), by Fred A. Demele and Ames Research Center (page images at HathiTrust)
• Importance of the variation of drag with lift in minimization of satellite entry acceleration (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers (National Aeronautics and Space Administration, 1959), by William A. McGowan and Langley Research Center (page images at HathiTrust)
• Creep bending and buckling of thin circular cylindrical shells (National Aeronautics and Space Administration, 1960), by Burton Erickson and Polytechnic Institute of Brooklyn (page images at HathiTrust)
• Investigation of methods for computing flutter characteristics of supersonic delta wings and comparison with experimental data (National Aeronautics and Space Administration, 1959), by Charles H. Wilts and California Institute of Technology (page images at HathiTrust)
• Measured and predicted section wave drag coefficients at a Mach number of 1.6 for a delta wing with two airfoil sections (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• Statistical loads data for the Airbus A-320 aircraft in commercial operations (Federal Aviation Administration, Office of Aviation Research ;, 2002), by John W. Rustenburg, Daniel O. Tipps, Donald A. Skinn, University of Dayton. Research Institute. Structural Integrity Division, William J. Hughes Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Statistical loads data for MD-82/83 aircraft in commercial operations (Federal Aviation Administration, Office of Aviation Research ;, 1999), by Donald Skinn, John Rustenburg, Daniel O. Tipps, University of Dayton. Research Institute. Structural Integrity Division, United States Federal Aviation Administration, and United States. Office of Aviation Research (page images at HathiTrust)
• An evaluation of methods to separate maneuver and gust load factors from measured acceleration time histories (U.S. Federal Aviation Administration, Office of Aviation Medicine ;, 1999), by John W. Rustenburg, Daniel O. Tipps, Donald A. Skinn, University of Dayton. Research Institute. Structural Integrity Division, United States Federal Aviation Administration, and United States. Office of Aviation Research (page images at HathiTrust)

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