Aerodynamic configurationsSee also what's at your library, or elsewhere.
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Filed under: Aerodynamic configurations Flight test results pertaining to the Space Shuttlecraft : a symposium held at Flight Research Center, Edwards, Calif., June 30, 1970. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Flight Research Center (U.S.) (page images at HathiTrust) Experimental investigation of model variable-geometry and ogee tip rotors / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Anton J. Landgrebe, E. Dean Bellinger, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust) Effects of canard planform and wing-leading-edge modification on low-speed longitudinal aerodynamic characteristics of a canard airplane configuration / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Bernard Spencer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) A viscous/potential flow interaction analysis method for multi-element infinite swept wings. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust) Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1970), by Langley Research Center and Douglas Aircraft Company (page images at HathiTrust) Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by William D. Beasley, Robert J. McGhee, and Langley Research Center (page images at HathiTrust) Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Gene J. Bingham, Kevin W. Noonan, and Langley Research Center (page images at HathiTrust) An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Harry H. Heyson and Langley Research Center (page images at HathiTrust) Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Ross B. Robinson and Langley Research Center (page images at HathiTrust) Wind-tunnel investigation of effect of ratio of wing chord to propeller diameter with addition of slats on the aerodynamic characteristics of tilt-wing VTOL configurations in the transition speed range / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Robert T. Taylor, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Ronald Tambor and Flight Research Center (U.S.) (page images at HathiTrust) FREE-FLIGHT AERODYNAMIC-HEATING DATA TO MACH NUMBER 10.4 FOR A MODIFIED VON KARMAN NOSE SHAPE. (Ft. Belvoir Defense Technical Information Center, MAY 1961), by COLLIE,KATHERINE A, BLAND,WILLIAM M JR, and NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C. (page images at HathiTrust; US access only)
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