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Short take-off and landing aircraft -- Design and construction

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• Short take-off and landing aircraft
• Airplanes -- Design and construction
• Fan-in-wing aircraft -- Design and construction
• Design and construction

• Vertically rising 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)

• 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)

• 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)

• Report of the Panel to Review the V-22 Program : hearing before the Committee on Armed Services, United States Senate, One Hundred Seventh Congress, first session, May 1, 2001. (U.S. G.P.O. :, 2002), by United States Senate Committee on Armed Services and United States. Panel to Review the V-22 Program (page images at HathiTrust)
• Report of the Panel to Review the V-22 Program : hearing before the Committee on Armed Services, United States Senate, One Hundred Seventh Congress, first session, May 1, 2001. (U.S. G.P.O. :, 2002), by United States Senate Committee on Armed Services and United States. Panel to Review the V-22 Program (page images at HathiTrust)

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

• The helicopter and other V/STOL aircraft in commercial transport service: growth to date and forecasted growth to 1965 and 1970. (Federal Aviation Agency, 1960), by United States. Federal Aviation Agency. Office of Plans (page images at HathiTrust)
• A technical summary and compilation of characteristics and specifications on steep-gradient aircraft; [Project Hummingbird, technical report] (U. S. Govt. Print. Off., 1961), by United States. Federal Aviation Agency (page images at HathiTrust)
• Safety through steep gradient aircraft : a survey of the status and effects of vertical and near-vertical take-off and landing (Daniel and Florence Guggenheim Aviation Safety Center, 1955), by Cornell University. Daniel and Florence Guggenheim Aviation Safety Center (page images at HathiTrust)
• Safety through steep gradient aircraft : supplement to 1955 survey reviewing status and special problems of vertical (VTOL) and short (STOL) take-off and landing types of aircraft (Daniel & Florence Guggenheim Aviation Safety Center at Cornell University, 1956), by R. M. Woodham and Cornell University. Daniel and Florence Guggenheim Aviation Safety Center (page images at HathiTrust)
• The Dupont Aerospace DP-2 aircraft : hearing before the Subcommittee on Investigations and Oversight of the Committee on Science and Technology, House of Representatives, One Hundred Tenth Congress, first session, June 12, 2007. (U.S. G.P.O. :, 2008), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight (page images at HathiTrust)
• The aerodynamic appraisal of STOL/VTOL configurations (Cornell Aeronautical Laboratory, 1960), by Robert J. Vidal, Richard A. Hartunian, and A. Sowyrda (page images at HathiTrust)
• Federal short takeoff and landing transport programs : status and needs, Department of Transportation, National Aeronautics and Space Administration, Department of Defense : report to the Congress (U.S. General Accounting Office, 1976), by United States General Accounting Office (page images at HathiTrust)
• Powered-lift aircraft technology (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1989), by W. H. Deckert, James A. Franklin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• A Review of technologies applicable to low-speed flight of high-performance aircraft investigated in the Langley 14- by 22-foot subsonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by John W. Paulson and Langley Research Center (page images at HathiTrust)
• Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Richard J. Re, George T. Carson, and Langley Research Center (page images at HathiTrust)
• Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), by W. S. Hindson, Robert C. Innis, Gordon H. Hardy, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Mary L. Mason, James R. Burley, and Langley Research Center (page images at HathiTrust)
• Aerodynamic analysis of several high throat Mach number inlets for the Quiet Clean Short-Haul Experimental Engine (National Aeronautics and Space Administration ;, 1975), by James A. Albers, John J. Hirn, Norbert O. Stockman, and Lewis Research Center (page images at HathiTrust)
• Low-speed wind tunnel tests of a 50.8-centimeter (20-in.) 1.15-pressure-ratio fan engine model (National Aeronautics and Space Administration ;, 1974), by Howard L. Wesoky and Lewis Research Center (page images at HathiTrust)
• Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85 (National Aeronautics and Space Administration ;, 1974), by Fred W. Steffen and Lewis Research Center (page images at HathiTrust)
• Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects (National Aeronautics and Space Administration ;, 1974), by Garl L. Gentry and Langley Research Center (page images at HathiTrust)
• Summary of recent short-haul systems studies (National Aeronautics and Space Administration, 1975), by Raymond C. Savin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of the VFR and IFR landing approach characteristics and terminal area airspace requirements for a light STOL airplane (National Aeronautics and Space Administration ;, 1974), by Harold L. Crane, Bruce D. Fisher, Kenneth R. Yenni, and Langley Research Center (page images at HathiTrust)
• Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by P. Frank Quinto, John W. Paulson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap (National Aeronautics and Space Administration ;, 1974), by William G. Johnson, Gerald E. Kardas, and Langley Research Center (page images at HathiTrust)
• Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (National Aeronautics and Space Administration ;, 1974), by George W. Lewis, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles (National Aeronautics and Space Administration, 1984), by H. C. Kao, Albert L. Johns, Paul L. Burstadt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Paul L. Coe, Donald R. Riley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Pressure distributions on a rectangular aspect-ratio-6, slotted supercritical airfoil wing with externally blown flaps (U.S. National Aeronautics and Space Administration ;, 1976), by William G. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a low-pressure fan stage with reverse flow (National Aeronautics and Space Administration ;, 1976), by Royce D. Moore, Edward R. Tysl, George W. Lewis, and Lewis Research Center (page images at HathiTrust)
• Performance of low-pressure ratio fan stage at two off-design blade setting (National Aeronautics and Space Administration ;, 1977), by George Kovich, Royce D. Moore, Edward R. Tysl, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Donald R. Riley, Gautam H. Shah, Richard E. Kuhn, and Langley Research Center (page images at HathiTrust)
• V/STOL aircraft. (National Aeronautics and Space Administration, 1964), by National Aeronautics and Space Administration (page images at HathiTrust)
• Effect on fan flow characteristics of length and axial location of a cascade thrust reverser (National Aeronautics and Space Administration ;, 1975), by Donald A. Dietrich, Gary G. Kelm, Andrew J. Crooker, and Lewis Research Center (page images at HathiTrust)
• A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Ames Research Center, Richard F. Vomaske, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model (National Aeronautics and Space Administration ;, 1975), by Danny R. Hoad and Langley Research Center (page images at HathiTrust)
• Three methods of presenting flight vector information in a head-up display during simulated STOL approaches (National Aeronautics and Space Administration ;, 1975), by James H. Dwyer, Everett A. Palmer, and Ames Research Center (page images at HathiTrust)
• Effect of entry-lip design on aerodynamics and acoustics of high-throat-Mach-number inlets for the quiet, clean, short-haul experimental engine (National Aeronautics and Space Administration ;, 1975), by Brent A. Miller, Howard L. Wesoky, and Benjamin J. Dastoli (page images at HathiTrust)
• Flight evaluation of stabilization and command augmentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by James A. Franklin, Gordon H. Hardy, Robert C. Innis, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics (National Aeronautics and Space Administration ;, 1971), by Julian Wolkovitch, D. William Lochtie, Charles W. LaMont, Lewis Research Center, and inc Mechanics Research (page images at HathiTrust)
• Conceptual design study of 1985 commercial tilt rotor transports : volume III--Stol design summary (U.S. National Aeronautics and Space Administration ;, 1976), by K. W. Sambell, United States National Aeronautics and Space Administration, and Bell Helicopter Company (page images at HathiTrust)
• Study of quiet turbofan STOL aircraft for short haul transportation (National Aeronautics and Space Administration, 1973), by T. P. Higgins, H. S. Sweet, E. G. Stout, Lockheed-Georgia Company, Lockheed-California Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Economic assessment of Short Takeoff and Landing aircraft potential including terminal area environmental considerations (National Aeronautics and Space Administration ;, 1974), by H. L. Solomon, Saul Sokolsky, Ames Research Center, and Aerospace Corporation (page images at HathiTrust)
• Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78 (National Aeronautics and Space Administration ;, 1977), by O. D. Wells, Douglas Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA CR-2374 (National Aeronautics and Space Administration ;, 1974), by David L. Kleinman, William R. Killingsworth, Langley Research Center, inc Systems Control, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Calculation of the longitudinal aerodynamic characteristics of wing-flap configurations with externally blown flaps (National Aeronautics and Space Administration ;, 1976), by M. R. Mendenhall, Langley Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Airworthiness criteria development for powered-lift aircraft : a program summary (National Aeronautics and Space Administration ;, 1977), by Robert K. Heffley, Robert C. Rumold, Robert L. Stapleford, inc Systems Technology, United States Federal Aviation Administration, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A survey of general coverage NAVAIDS for V/STOL aircraft : a VOR/DME model (National Aeronautics and Space Administration, 1970), by Henry K. Johansen, United States National Aeronautics and Space Administration, Massachusetts Institute of Technology, and Electronics Research Center (page images at HathiTrust)
• STOL ride control feasibility study : technical report (National Aeronautics and Space Administration ;, 1973), by C. K. Gordon, R. O. Dodson, Langley Research Center, and Boeing Company. Wichita Division (page images at HathiTrust)
• Feasibility of V/STOL concepts for short-haul transport aircraft (National Aeronautics and Space Administration, 1968), by Bernard L. Fry and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Michael R. Mendenhall, Selden B. Spangler, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1969), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-2014 (National Aeronautics and Space Administration, 1963), by Matthew M. Winston, Robert J. Huston, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Theoretical aerodynamics of upper-surface-blowing jet-wing interaction (National Aeronautics and Space Administration ;, 1975), by C. Edward Lan, James F. Campbell, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory (National Aeronautics and Space Administration ;, 1975), by Boyd Perry, George C. Greene, and Langley Research Center (page images at HathiTrust)
• NASA TN D-2231 (National Aeronautics and Space Administration :, 1964), by Hervey C. Quigley, Curt A. Holzhauser, Robert C. Innis, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2498 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Demo J. Giulianetti, Victor R. Corsiglia, James C. Biggers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions (National Aeronautics and Space Administration, 1967), by James R. Kelly, Perry L. Deal, John F. Garren, and Langley Research Center (page images at HathiTrust)
• Flight tests under IFR with an STOL transport aircraft (National Aeronautics and Space Administration ;, 1968), by Robert C. Innis, Richard P. Gallant, Curt A. Holzhauser, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a powered, externally blown flap STOL transport model with two engine simulator sizes (National Aeronautics and Space Administration ;, 1975), by William G. Johnson and Langley Research Center (page images at HathiTrust)
• Moving-base visual simulation study of decoupled controls during approach and landing of a STOL transport aircraft (National Aeronautics and Space Administration ;, 1975), by G. Kimball Miller, Perry L. Deal, and Langley Research Center (page images at HathiTrust)
• A flight investigation of piloting techniques and crosswind limitations during visual STOL-Type landing operations (National Aeronautics and Space Administration ;, 1976), by Langley Research Center, Bruce D. Fisher, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6161 (National Aeronautics and Space Administration ;, 1971), by Henry C. Haller, Bruce M. Auer, Seymour Lieblein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field length (National Aeronautics and Space Administration ;, 1976), by Jeffrey V. Bowles, Thomas L. Galloway, Mark H. Waters, and Ames Research Center (page images at HathiTrust)
• Flight-path and airspeed control during landing approach for powered-lift aircraft (National Aeronautics and Space Administration ;, 1974), by James A. Franklin, Robert C. Innis, and Ames Research Center (page images at HathiTrust)
• Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence (National Aeronautics and Space Administration ;, 1975), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles (National Aeronautics and Space Administration ;, 1975), by William C. Sleeman, William C. Hohlweg, and Langley Research Center (page images at HathiTrust)
• Analysis of a flare-director concept for an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), by David B. Middleton (page images at HathiTrust)
• Wind-tunnel investigation of internally blown jet-flap STOL airplane model (National Aeronautics and Space Administration :, 1976), by Raymond D. Vogler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee (National Aeronautics and Space Administration ;, 1977), by William C. Sleeman, Langley Research Center, United States National Aeronautics and Space Administration, and David R Forsyth (page images at HathiTrust)
• Real-time manned simulation of advanced terminal area guidance concepts for short-haul operations (National Aeronautics and Space Administration ;, 1977), by Leonard Tobias, Paul J. O'Brien, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simulation studies of STOL airplane operations in metropolitan downtown and airport air traffic control environments (National Aeronautics and Space Administration ;, 1974), by Richard H. Sawyer, Milton D. McLaughlin, and Langley Research Center (page images at HathiTrust)
• Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport (National Aeronautics and Space Administration :, 1970), by Joseph R. Chambers, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail (National Aeronautics and Space Administration, 1968), by Richard J. Margason, Garl L. Gentry, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model (National Aeronautics and Space Administration ;, 1969), by Arthur W. Carter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap (National Aeronautics and Space Administration :, 1969), by Lysle P. Parlett, James P. Shivers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of V/STOL transport model with six wing-mounted lift fans (National Aeronautics and Space Administration, 1970), by William A. Newsom, Frederick L. Moore, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6636 (National Aeronautics and Space Administration :, 1972), by William A. Olsen, Robert G. Dorsch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6710 (National Aeronautics and Space Administration :, 1972), by Frederick W. Gibson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Review of propulsion-induced effects on aerodynamics of jet/stol aircraft (National Aeronautics and Space Administration :, 1970), by Richard J. Margason, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Supersonic transport operating practices during simulated operations in future air traffic control system environments (National Aeronautics and Space Administration ;, 1969), by Milton D. McLaughlin, Richard H. Sawyer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane (National Aeronautics and Space Administration ;, 1974), by William D. Grantham, Perry L. Deal, Luat T. Nguyen, and Langley Research Center (page images at HathiTrust)
• Analytical study of takeoff and landing performance for a jet STOL transport configuration with full-span, externally blown, triple-slotted flaps (National Aeronautics and Space Administration ;, 1973), by Harold P. Washington, John T. Gibbons, and Flight Research Center (U.S.) (page images at HathiTrust)
• Computed lateral power spectral density response of conventional and STOL airplanes to random atmospheric turbulence (National Aeronautics and Space Administration ;, 1974), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• Lateral static and dynamic aerodynamic parameters of the Kestrel aircraft (XV-6A) extracted from flight data (National Aeronautics and Space Administration ;, 1974), by William T. Suit, James L. Williams, and Langley Research Center (page images at HathiTrust)
• Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing (National Aeronautics and Space Administration ;, 1973), by Bruce G. Powers, David A. Kier, and Flight Research Center (U.S.) (page images at HathiTrust)
• Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston. (National Aeronautics and Space Administration :, 1970), by Matthew M. Winston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Static and wind-on tests of an upper-surface-blown jet-flap nozzle arrangement for use on the Quiet Clean Shore-haul Experimental Engine (QCSEE) (National Aeronautics and Space Administration ;, 1977), by Arthur E. Phelps, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landing rates for mixed STOL and CTOL traffic (National Aeronautics and Space Administration ;, 1974), by John S. White and Ames Research Center (page images at HathiTrust)
• NASA TN D-4237 (National Aeronautics and Space Administration ;, 1967), by Kenneth W. Goodson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal aerodynamic characteristics in ground effect of a large-scale, V/STOL model with four tilting ducted fans arranged in a dual tandem configuration (National Aeronautics and Space Administration, 1967), by Demo J. Giullianetti, Ralph L. Maki, James C. Biggers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), by M. Leroy Spearman, Gerald V. Foster, and Langley Research Center (page images at HathiTrust)
• Results of full-scale wind tunnel tests on the H.126 jet flap aircraft (National Aeronautics and Space Administration ;, 1973), by Thomas N. Aiken, Anthony Cook, and Ames Research Center (page images at HathiTrust)
• A Flight investigation with STOL airplane flying curved, descending instrument approach paths (National Aeronautics and Space Administration ;, 1974), by Margaret S. Benner and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of a deflected-slipstream cruise-fan V/STOL aircraft wing (National Aeronautics and Space Administration, 1967), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1647 (National Aeronautics and Space Administration, 1963), by Hervey C. Quigley, Robert C. Innis, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model (National Aeronautics and Space Administration ;, 1971), by Charles C. Smith, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Airport-area airspace used in simulated operations with an experimental powered-lift STOL airplane (National Aeronautics and Space Administration ;, 1973), by Norman S. Silsby, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A compilation and analysis of typical approach and landing data for a simulator study of an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), by David B. Middleton, Hugh P. Bergeron, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6292 (National Aeronautics and Space Administration ;, 1971), by Kalman J. Grunwald, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Gust alleviation for a STOL transport by using elevator, spoilers, and flaps (National Aeronautics and Space Administration ;, 1974), by Frederick J. Lallman and Langley Research Center (page images at HathiTrust)
• Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep (National Aeronautics and Space Administration, 1960), by Arvo A. Luoma, William J. Alford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 degree (National Aeronautics and Space Administration, 1960), by Gerald V. Foster, Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground noise measurements during landing, take-off, and flyby operations of a four-engine turbopropeller STOL airplane (National Aeronautics and Space Administration ;, 1971), by David A. Hilton, Domenic J. Maglieri, Herbert R. Henderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio (National Aeronautics and Space Administration, 1971), by V. Robert Page, Thomas N. Aiken, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model (National Aeronautics and Space Administration ;, 1973), by James L. Thomas, Delwin R. Croom, Danny R. Hoad, and Langley Research Center (page images at HathiTrust)
• Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap (National Aeronautics and Space Administration ;, 1973), by Arthur R. Phelps, Robert L. Henderson, William Letko, and Langley Research Center (page images at HathiTrust)
• Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions (National Aeronautics and Space Administration ;, 1973), by James A. Albers and Lewis Research Center (page images at HathiTrust)
• Simulator study of minimum acceptable level of longitudinal stability for a representative STOL configuration during landing approach (National Aeronautics and Space Administration ;, 1974), by William D. Grantham, Perry L. Deal, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of a four-engine externally blowing jet-flap STOL airplane model. (National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1970), by Raymond D. Vogler, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model (National Aeronautics and Space Administration ;, 1973), by Charles Christian Smith and Langley Research Center (page images at HathiTrust)
• Analytical study of the performance of a gust alleviation system for a STOL airplane (National Aeronautics and Space Administration ;, 1973), by Waldo I. Oehman and Langley Research Center (page images at HathiTrust)
• Vertical and short takeoff and landing (V/STOL) aircraft. : Report of the Special Subcommittee on Research and Development of the Committee on Armed Services, House of Representatives, Eighty-eighth Congress, second session. (U.S. Govt. Print. Off, 1964), by United States House Committee on Armed Services (page images at HathiTrust)
• Civil Aeronautics Board planning study : STOL/VTOL air transportation systems (U.S. Civil Aeronautics Board, 1970), by Carl Hintze and United States. Civil Aeronautics Board. Bureau of Economics (page images at HathiTrust)
• Study on the feasibility of V/STOL concepts for short-haul transport aircraft (National Aeronautics and Space Administration ;, 1967), by Dallas Ling-Temco-Vought. Research Center and K. R. Marsh (page images at HathiTrust)
• Review of defense-related vertical and short takeoff and landing (V/STOL) aircraft programs : a staff study for the Committee on Armed Services, House of Representatives, Ninety-sixth Congress, first session (U.S. G.P.O., 1979), by Walter Z. Collings and United States House Committee on Armed Services (page images at HathiTrust)
• Composite V/STOL utility/logistics aircraft, speed versus payload and productivity (Aberdeen, Maryland : Aberdeen Proving Ground, 1967., 1967), by Roy C. Schmidt, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An analytical study of V/STOL handling qualities in hover and transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by Robert L. Stapleford, Inc Systems Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• YC-14 interior noise measurements program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by L. M. Butzel, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Commercial Airplane Company (page images at HathiTrust)
• Predictive methods for the dynamic response of a quad tilt-duct V/STOL aircraft in transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by Irving Carl Statler, A. Sowyrda, J. C. Erickson, G. Kurylowich, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Aerodynamic stability and control/wind tunnel data correlation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by G. R. Casteel, Air Force Flight Dynamics Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Proceedings : ejector workshop for aerospace applications (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by R. P. Braden, H. J. P. von Ohain, K. S. Nagaraja, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
• Investigation of the effects of gusts on V/STOL craft in transition and hover (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by Grant Brandford Skelton, Air Force Flight Dynamics Laboratory (U.S.), and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• A flight investigation of lateral-directional handling qualities for V/STOL aircraft in low speed maneuvering flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by K. H. Doetsch, D. M. McGregor, D. G. Gould, Air Force Flight Dynamics Laboratory (U.S.), and National Aeronautical Establishment (Canada) (page images at HathiTrust)
• Tentative STOL flying qualities criteria for MIL standard and handbook (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Roger H. Hoh, David G. Mitchell, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• An investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), by Travis W. Binion, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• An Experimental study of several wind tunnel wall configurations using two V/STOL model configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), by T. W. Binion, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• An Empirical method for estimating the effect of ground proximity on the jet-induced lift of VSTOL aircraft employing rectangular jets (Warminster, Pennsylvania : Naval Air Development Center, 1981., 1981), by J. A. Sansone, General Dynamics Corporation. Fort Worth Division, and Naval Air Development Center (page images at HathiTrust)
• STOL tactical aircraft investigation - externally blown flap. Volume III, Performance methods and takeoff and landing rules (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Dirk J. Renselaer, Air Force Flight Dynamics Laboratory (U.S.), Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Prediction methodology for propulsive induced forces and moments in transtion/STOL flight. Volume I, Technical discussions (Warminster, Pennsylvania : Naval Air Development Center, 1979., 1979), by T. D. Beatty, S. S. Kress, Vought Corporation, and Naval Air Development Center (page images at HathiTrust)
• A laboratory investigation into flight path perturbations during steep descents of V/STOL aircraft (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1976), by L. D. Reid, Peter C. Hughes, H. W. Teunissen, Bernard Etkin, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)
• Lift system induced aerodynamics of V/STOL aircrtaft in a moving deck environment. Volume II, Static and dynamic jet-induced force and moment data (Warminster, Pennsylvania : Naval Air Development Center, 1978., 1978), by James H. Kamman, Charles L. Hall, McDonnell Aircraft Company, and Naval Air Development Center (page images at HathiTrust)
• An analysis of fixed wing-proprotor interference for folding proprotor aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Carl G. Matthys, P. Y. Hsieh, Mukund M. Joglekar, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Bell Helicopter Company (page images at HathiTrust)

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