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Transport planes -- Wings -- Design and construction

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Filed under: Transport planes -- Wings -- Design and construction

NASA TN D-1809 (National Aeronautics and Space Administration, 1963), by Richard J. Re, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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

Filed under: Transport planes -- Wings -- Aerodynamics

NASA TN D-1809 (National Aeronautics and Space Administration, 1963), by Richard J. Re, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

Filed under: Airplanes -- Wings -- Design and construction

Établissement, calcul et construction des surfaces portantes. (Librairie aéronautique, 1914), by Paul James (page images at HathiTrust; US access only)
Large-scale static investigation of circulation-control-wing concepts applied to upper-surface-blowing aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by M. D. Shovlin and Ames Research Center (page images at HathiTrust)
Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by H. Paul Stough, James M. Patton, Daniel J. DiCarlo, and Langley Research Center (page images at HathiTrust)
Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert J. Mack and Langley Research Center (page images at HathiTrust)
A method for the design of transonic flexible wings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Leigh Ann Smith, Richard L. Campbell, and Langley Research Center (page images at HathiTrust)
Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Charles L. Ruhlin, K. S. Nagaraja, Kumar G. Bhatia, and Langley Research Center (page images at HathiTrust)
Effect of leading-edge load constraints on the design and performance of supersonic wings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Christine M. Darden and Langley Research Center (page images at HathiTrust)
Investigation of the applicability of the free-wing principle to light, general aviation aircraft (National Aeronautics and Space Administration ;, 1972), by Richard F. Porter, Joe H. Brown, Ross G. Luce, Langley Research Center, and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust)
Study of advanced composite structural design concepts for an arrow wing supersonic cruise configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by M. J. Turner, D. L. Grande, Langley Research Center, Boeing Commercial Airplane Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
NASA TR R-152 (National Aeronautics and Space Administration ;, 1963), by Clarence D. Cone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Natural laminar flow airfoil design considerations for winglets on low-speed airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by C. P. Van Dam, Langley Research Center, and Vigyan Research Associates (page images at HathiTrust)
NASA TN D-4427 (National Aeronautics and Space Administration ;, 1968), by John E. Lamar, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5805 (National Aeronautics and Space Administration :, 1970), by Edward J. Ray, Robert T. Taylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-4493 (National Aeronautics and Space Administration ;, 1968), by Stanley O. Dickinson, W. H. Deckert, V. Robert Page, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Numerical methods for the design and analysis of wings at supersonic speeds (National Aeronautics and Space Administration ;, 1974), by Harry W. Carlson, David S. Miller, and Langley Research Center (page images at HathiTrust)
An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds (National Advisory Committee for Aeronautics, 1955), by Robert R. Howell, Albert L. Braslow, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations (National Aeronautics and Space Administration, 1959), by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
Preliminary design of wings. Volume III, Minimum weight design of stiffened plate (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
Preliminary design of wings. Volume IV, Minimum weight design of composite structure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
Preliminary design of wings. Volume I, Design philosophy (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
Preliminary design of wings. Volume II, Preliminary fatigue design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
Analysis/Theory of controlled configured structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by J. G. Williams, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)

Filed under: Airplanes -- Wings -- Design and construction -- Computer programs

A transonic-small-disturbance wing design methodology (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Pamela S. Phillips, Richard L. Campbell, Edgar G. Waggoner, and Langley Research Center (page images at HathiTrust)
WIDOWAC (Wing Design Optimization with Aeroelastic Constraints) : program manual (National Aeronautics and Space Administration ;, 1974), by Raphael T. Haftka, James H. Starnes, and Langley Research Center (page images at HathiTrust)
Application of mathematical optimization procedures to a structural model of a large finite-element wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Joanne L. Walsh and Langley Research Center (page images at HathiTrust)
Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1990), by Gregory A. Wrenn, Augustine R. Dovi, Langley Research Center, and Lockheed Engineering & Sciences Company (page images at HathiTrust)
Automated procedure for design of wing structures to satisfy strength and flutter requirements (National Aeronautics and Space Administration ;, 1973), by Raphael T. Haftka and Langley Research Center (page images at HathiTrust)

Filed under: Airplanes -- Wings -- Design and construction -- Data processing

Computer-aided space shuttle orbiter wing design study (National Aeronautics and Space Administration ;, 1974), by W. Pelham Phillips and Langley Research Center (page images at HathiTrust)

Filed under: Airplanes -- Wings -- Design and construction -- Mathematical models

Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by John DeYoung, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

Filed under: Fan-in-wing aircraft -- Design and construction

V/STOL lift fan commercial short-haul transports : continuing conceptual design study (National Aeronautics and Space Administration ;, 1974), by J. M. Zabinsky, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)

Filed under: Short take-off and landing aircraft -- Design and construction

Conceptual design study of improved 1985 remote lift-fan V/Stol commercial transports (National Aeronautics and Space Administration ;, 1975), by Robert L. Cavage, Ames Research Center, and Rockwell International (page images at HathiTrust)
Conceptual design studies of a V/STOL civil lift fan transport including effect of size and fan pressure ratio. (National Aeronautics and Space Administration ;, 1974), by Ames Research Center and McDonnell Aircraft Company (page images at HathiTrust)
Evaluation of advanced lift concepts and potential fuel conservation for short-haul aircraft (National Aeronautics and Space Administration ;, 1975), by H. S. Sweet, M. K. Bowden, J. H. Renshaw, Ames Research Center, and Lockheed Aircraft Corporation (page images at HathiTrust)
V/STOL lift fan commercial short-haul transports : continuing conceptual design study (National Aeronautics and Space Administration ;, 1974), by J. M. Zabinsky, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
Conceptual engineering design studies of 1985-era commercial VTOL and STOL transports that utilize rotors (National Aeronautics and Space Administration ;, 1975), by J. P. Magee, Colin A. Widdison, R. D. Clark, Ames Research Center, and Boeing Vertol Company (page images at HathiTrust)
Conceptual design studies of candidate V/STOL lift fan commercial short haul transport for 1980-85 V/STOL lift fan study (National Aeronautics and Space Administration ;, 1973), by William M. Eldridge, Ames Research Center, and Boeing Company (page images at HathiTrust)
NASA TN D-4448 (National Aeronautics and Space Administration ;, 1968), by V. Robert Page, W. H. Deckert, Stanley O. Dickinson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Acoustic and aerodynamic performance of 1.83-meter (6-ft) diameter 1.25-pressure-ratio fan (QF-8) (U.S. National Aeronautics and Space Administration, Lewis Research Center ;, 1976), by Richard P. Woodward, James G. Lucas, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
NASA TN D-5481 (National Aeronautics and Space Administration ;, 1969), by Marvin P. Fink, Charles C. Smith, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration (National Aeronautics and Space Administration ;, 1975), by Arthur E. Phelps and Langley Research Center (page images at HathiTrust)
Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume II, STOL aerodynamic methods computer program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by M. I. Goldhammer, N. F. Wasson, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume III, Engineering methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by M. I. Goldhammer, M. L. Lopez, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)

Filed under: Vertically rising aircraft -- Design and construction

Conceptual design study of 1985 commercial VTOL transports that utilize rotors : summary (National Aeronautics and Space Administration ;, 1975), by N. F. K. Kefford, C. L. Munch, Ames Research Center, and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)
Conceptual design study of improved 1985 remote lift-fan V/Stol commercial transports (National Aeronautics and Space Administration ;, 1975), by Robert L. Cavage, Ames Research Center, and Rockwell International (page images at HathiTrust)
Conceptual design studies of a V/STOL civil lift fan transport including effect of size and fan pressure ratio. (National Aeronautics and Space Administration ;, 1974), by Ames Research Center and McDonnell Aircraft Company (page images at HathiTrust)
V/STOL lift fan commercial short-haul transports : continuing conceptual design study (National Aeronautics and Space Administration ;, 1974), by J. M. Zabinsky, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
Conceptual engineering design studies of 1985-era commercial VTOL and STOL transports that utilize rotors (National Aeronautics and Space Administration ;, 1975), by J. P. Magee, Colin A. Widdison, R. D. Clark, Ames Research Center, and Boeing Vertol Company (page images at HathiTrust)
Conceptual design studies of candidate V/STOL lift fan commercial short haul transport for 1980-85 V/STOL lift fan study (National Aeronautics and Space Administration ;, 1973), by William M. Eldridge, Ames Research Center, and Boeing Company (page images at HathiTrust)
Conceptual design study of a V/STOL lift fan commercial short haul transport (National Aeronautics and Space Administration ;, 1973), by Ronald G. Knight, Jerome A. Prizlow, William V. Powell, Ames Research Center, and North American Rockwell Corporation (page images at HathiTrust)
NASA TN D-5481 (National Aeronautics and Space Administration ;, 1969), by Marvin P. Fink, Charles C. Smith, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-3213 (National Aeronautics and Space Administration ;, 1966), by Raymond D. Vogler, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
NASA TN D-4084 (National Aeronautics and Space Administration ;, 1967), by Kenneth P. Spreemann, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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