The Online Books Page

Vertically rising aircraft -- Statistics

See also what's at your library, or elsewhere.

• Vertically rising aircraft
• Short take-off and landing aircraft -- Statistics
• Statistics

• Vertically rising aircraft -- Aerodynamics -- Statistics

• Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1974), by Raymond E. Mineck, Richard J. Margason, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range (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)

• Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1973), by Raymond E. Mineck, Myles F. Schwendemann, and Langley Research Center (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)
• Simulation of helicopter and V/STOL aircraft (Obtainable from Defense Documentation Center], 1963), by Inc. Melpar, Merlin P. Coffee, Walter McIntyre, and James R. Toler (page images at HathiTrust; US access only)
• Theoretical and experimental studies of impinging uniform jets. Task 1D121401A14129, (formerly Task 9R38-01-017-29) Contract DA44-177-TC-782. (Available from Armed Services Technical Information Agency], 1963), by Cornell Aeronautical Laboratory (page images at HathiTrust)
• Performance and stresses obtained on an isolated VTOL-type propeller operating in hovering, transitional and axial flight (U. S. Army Aviation Material Laboratories, 1967), by Andrew Richard Trenka and Cornell Aeronautical Laboratory (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)
• 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)
• 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)
• An assessment of the capability to calculate tilting prop-rotor aircraft performance, loads, and stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Wayne Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by J. Dennis Hawk, Norbert O. Stockman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (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)
• Study on the feasibility of V/STOL concepts for short haul transport aircraft (National Aeronautics and Space Administration, 1967), by Lockheed-California Company (page images at HathiTrust)
• Recirculation characteristics of a small-scale VTOL lift engine pod (National Aeronautics and Space Administration, 1971), by Gordon H. Hall, United States National Aeronautics and Space Administration, Lewis Research Center, and Northrop Corporation (page images at HathiTrust)
• Model tests of concepts to reduce hot gas ingestion in VTOL lift engines (National Aeronautics and Space Administration, 1971), by Gordon R. Hall, United States National Aeronautics and Space Administration, Lewis Research Center, and Northrop Corporation (page images at HathiTrust)
• A technique for generating arbitrarily shaped curved approach paths (National Aeronautics and Space Administration ;, 1976), by Walter J. McConnell, Langley Research Center, and Sperry Flight Systems (Firm) (page images at HathiTrust)
• Experimental investigation of a 4 1/2-stage turbine with very high stage loading factor (National Aeronautics and Space Administration ;, 1973), by D. C. Evans, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Scaling of VTOL recirculation effects (National Aeronautics and Space Administration, 1970), by Gordon R. Hall, United States National Aeronautics and Space Administration, Lewis Research Center, and Northrop Corporation (page images at HathiTrust)
• Static performance of a 13.97-cm (5.5-inch) diameter model VTOL lift fan (National Aeronautics and Space Administration ;, 1972), by W. H. Lowe, R. W. Sanger, Lewis Research Center, and General Dynamics Corporation (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)
• Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models (National Aeronautics and Space Administration, 1968), by Ray H. Wright, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Flight investigation of stability and control characteristics of a 1/9-scale model of a four-propeller tilt-wing v/stol transport (National Aeronautics and Space Administration, 1964), by William A. Newsom, Robert H. Kirby, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-2680 (National Aeronautics and Space Administration, 1965), by Robert J. Pegg, John P. Reeder, Henry L. Kelley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of a direct side-force maneuvering system on a deflected jet VTOL aircraft (National Aeronautics and Space Administration, 1969), by Terrell W. Feistel, Emmett B. Fry, Robert M. Gerdes, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Analysis of 2-D inviscid model of jet impingement under vertical-takeoff airplane (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Robert Siegel, Marvin E. Goldstein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5256 (National Aeronautics and Space Administration ;, 1969), by Robert J. Huston, James P. Shivers, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• 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)
• Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests (National Aeronautics and Space Administration, 1968), by Joseph R. Chambers, Sue B. Grafton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6198 (National Aeronautics and Space Administration ;, 1971), by William A. Newsom, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (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)
• Wing-surface-jet interaction characteristics of an upper-surface blown model with rectangular exhaust nozzles and a radius flap (National Aeronautics and Space Administration ;, 1976), by Alvin M. Bloom, William C. Sleeman, William C. Hohlweg, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical analysis of flow in VTOL lift fan inlets without crossflow (National Aeronautics and Space Administration, 1969), by Norbert O. Stockman, Seymour Lieblein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of various small-scale rotor/wing configurations for VTOL composite aircraft in the cruise mode (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by James P. Shivers (page images at HathiTrust; US access only)
• Comparison of information display concepts for landing of VTOL aircraft (National Aeronautics and Space Administration, 1968), by William Gracey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5491 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by L. Stewart Rolls, Ronald M. Gerdes, Ames 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)
• NASA TN D-5581 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by H. Clyde McLemore, Patricia G. Hemeter, Charles C. Smith, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks (National Aeronautics and Space Administration ;, 1969), by Emmett B. Fry, Ronald M. Gerdes, Richard K. Greif, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• NASA TN D-5342 (National Aeronautics and Space Administration :, 1969), by Frank R. Niessen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of the optimum values of several parameters affecting longitudinal handling qualities of VTOL aircraft (National Aeronautics and Space Administration, 1968), by James R. Kelly, John F. Garren, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Flight investigation of a vertical-velocity command system for VTOL aircraft (National Aeronautics and Space Administration ;, 1977), by James R. Kelly, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted life-cruise engines for propulsion (National Aeronautics and Space Administration, 1967), by Jerry V. Kirk, Leo P. Hall, Brent K. Hodder, United States National Aeronautics and Space Administration, 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)
• Static and dynamic longitudinal stability derivatives of a powered 0.18 scale model of a fan-in-wing VTOL aircraft (National Aeronautics and Space Administration, 1968), by Joseph R. Chambers, Sue B. Grafton, Langley Research Center, 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)
• NASA TN D-1629 (National Aeronautics and Space Administration, 1963), by Raymond D. Vogler, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Investigation of the effect of downwash from a vertical takeoff and landing aircraft and a helicopter in the ground environment (National Aeronautical and Space Administration, 1961), by Thomas C. O'Bryan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model (National Aeronautics and Space Administration ;, 1969), by Matthew M. Winston, Robert J. Huston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6234 (National Aeronautics and Space Administration ;, 1971), by Stanley O. Dickinson, Brent K. Hodder, Leo P. Hall, United States National Aeronautics and Space Administration, and Ames 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)
• The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model (National Aeronautics and Space Administration ;, 1974), by Harry H. Heyson 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)
• 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)
• Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90©� (National Advisory Committee for Aeronautics, 1954), by John W. Draper, Richard E. Kuhn, and United States National Advisory Committee for Aeronautics (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)
• The design of a supersonic V/STOL fighter-bomber. (Bell Aerosystems Co., 1961), by James Aloysius O'Malley (page images at HathiTrust)
• A compilation of the papers presented : Langley Research Center, Langley Field, Va., November 17-18, 1960. (National Aeronautics and Space Administration, 1960), by Va.) NASA Conference on V/STOL aircraft (1960 : Langley Field (page images at HathiTrust)
• Outlook for vertical-lift aircraft in scheduled commercial transportation. (Cambridge, 1963), by inc United Research (page images at HathiTrust; US access only)
• An early overview of tiltrotor aircraft characteristics and pilot procedures in civil transport applications (Federal Aviation Administration, Advanced System Design Service ;, 1989), by David L. Green, Michael Saraniero, Harold Andrews, Starmark Corporation, and United States. Federal Aviation Administration. Advanced System Design Service (page images at HathiTrust)
• Application of tiltrotor technology to U.S. Coast Guard missions (U.S. Coast Guard, Office of Engineering, Logistics, and Development ;, 1993), by J. Casler, U.S. Coast Guard Research & Development Center, and Logistics United States. Coast Guard. Office of Engineering (page images at HathiTrust)
• A strategy for advancing tilt-rotor technology : final report (Ames Research Center, 1985), by Edward K. Morlok, David L. Schoendorfer, Ames Research Center. Powered Lift Flight Investigation Branch, Ames Research Center, University of Pennsylvania. Transportation Program, and University of Pennsylvania. Dept. of Civil Engineering (page images at HathiTrust)
• Effects of civil tiltrotor service in the Northeast corridor on en route airspace loads (Federal Aviation Administration, Operations Research Service ;, 1994), by William W. Trigeiro, Stephanie B. Fraser, Xavier P. Szebrat, Mitre Corporation, and United States. Federal Aviation Administration. Operations Research Service (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume III, Additional data for two-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (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)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 2, Additional data for the one-jet configuration (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• A method for estimating damping derivatives of VTOL aircraft in transition and hovering flight (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by Paiewonsky Bernard H., United States. Air Force. Air Research and Development Command, and Wright Air Development Center (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)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 4, Additional data for three-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (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)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 1, Test description and data analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (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)
• Application of the vortex-lattice method to represent a jet exhausting from a flat plate into a crossflowing stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by F. L. Heltsley, R. L. Parker, Martin Marietta Corporation, McDonnell Douglas Corporation, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• An Experimental investigation of VTOL flying qualities requirements for shipboard landings (Warminster, Pennsylvania : Naval Air Development Center, 1981., 1981), by Robert C. Radford, John L. Beilman, Dominick Andrisani, Calspan 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)
• 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)
• Structural dynamic response of large logistic V/STOL vehicles. (AF Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1964), by United Aircraft Corporation. Sikorsky Aircraft Division, M. J. Rich, and Air Force Flight Dynamics Laboratory (U.S.) Research and Technology Division (page images at HathiTrust)

More items available under broader and related terms at left.