The Online Books Page

Aircraft configurations

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• Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 3.96 and 4.63 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Maurice O. Feryn and Langley Research Center (page images at HathiTrust)
• Investigation of double slotted flaps on a swept-wing transport model / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Rodger L. Naeseth, Edwin E. Davenport, and Langley Research Center (page images at HathiTrust)
• Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
• The interpretation of nonlinear pitching moments in relation to the pitch-up problem / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by George S. Campbell, Joseph Weil, and Langley Research Center (page images at HathiTrust)
• Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Clarence L. Gillis, A. James Vitale, and Langley Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by David G. Koenig, Mark W. Kelly, Richard K. Greif, and Ames Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of blowing boundary-layer control on leading- and trailing-edge flaps of a full-scale, low-aspect-ratio, 42° swept-wing airplane configuration / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Ralph L. Maki, Demo J. Giulianetti, and Ames Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.