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Stability and control

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• An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles F. Whitcomb, Chris C. Critzos, Philippa F. Brown, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by / (Washington, D.C. : National Aeronautics and Space Administration :, 1959), by John W. Paulson, Robert E. Shanks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pressure loads produced on a flate-plate wing by rocket jets exhausting in a spanwise direction below the wing and perpendicular to a free-stream flow of mach number 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ralph A. Falanga, Joseph J. Janos, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John F. Garren and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static aerodynamic characteristics of a two-stage and a three-stage rocket vehicle at Mach numbers from 1.47 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce,], [1962]), by Clarence A. Brown, Ausley B. Carraway, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical approach to the design of an automatic discontinuous control system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rotational decay of the satellite 1960 ETA 2 due to the Earth's magnetic field. / Raymond H. Wilson, Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Raymond H. Wilson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Induced interference effects on jet and buried-fan VTOL configurations in transtition / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Handling qualities experience with several VTOL research aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John P. Reeder and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic interaction effects ahead of a sonic jet exhausting perpendicularly from a flat plate into a mach number 6 free stream / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by David J. Romeo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight controllability limits and related human transfer functions as determined from simulator and flight tests / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lawrence W. Taylor, Richard E. Day, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of ratio of jet area to total area and of pressure on lift augmentation of annular jets in ground effect under static conditions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Kenneth W. Goodson, James H. Otis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Launch characteristics of the X-15 research airplane as determined in flight / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gene J. Matranga and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ground interference effects / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert O. Schade and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of propeller-driven VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a low-thrust storable propellant rocket at very low chamber pressure / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John P. Wanhainen, Phil S. Ross, Richard L. DeWitt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of systems using inertia wheels for precise attitude control of a satellite / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John S. White, Q. Marlon Hansen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Russell L. Schott and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of wind compensation for launching of unguided rockets. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert L. James and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by George M. Ware and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Loads induced on a flat-plate wing by an air jet exhausting perpendicularly through the wing and normal to a free-stream flow of mach number 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph J. Janos and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by L. Stewart Rolls, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Secondary flow fields embedded in hypersonic shock layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Alvin Seiff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bruce E. Tinling, Clyde Q. Allen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interaction of highly underexpanded jets with simulated lunar surfaces / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Leonard E. Stitt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of solar radiation pressure on the motion of an artificial satellite / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert W. Bryant and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Roxanah B. Yancey and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert L. Gungle, H. Wayne Leonard, William S. Brosier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a proposed infrared horizon scanner for use in space-orientation control systems / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Norman M. Hatcher, Ernst F. Germann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by James S. Bowman, William D. Grantham, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles C. Smith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gene J. Matranga and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of an airplane model with an unswept, tilt wing of aspect ration 5.5, and with four propellers and blowing flaps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James A. Weiberg, Curt A. Holzhauser, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic aerodynamic characteristics of a wing-body combination having a 52.2⁰ sweptback wing of aspect ratio 3 with conical camber and designed for a mach number of 2/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William B. Igoe, Maarlowe D. Cassetti, Richard J. Re, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Kenneth Margolis, Miriam H. Elliott, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Victor L. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tests of an asymmetrical baffle for fuel-sloshing suppression / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Henry A. Cole, Bruno J. Gambucci, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of the aerodynamic characteristics of a fixed geometry paraglider configuration and three canopies with simulated variable canopy inflation at a mach number of 6.6 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Jim A. Penland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Equations of motion and design criteria for the despin of a vehicle by the radial release of weights and cables of finite mass / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald G. Elde, Chester A. Vaughan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by David G. Koenig, James A. Brady, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight study of the conversion maneuver of a tilt-duct VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Robert J. Tapscott, Henry L. Kelley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of a pilot-airplane lateral instability experienced with the X-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lawrence W. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Predicted performance of on-off systems for precise satellite attitude control / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Stuart C. Brown and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel tests of a 1/20-scale airship model with stern propellers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by H. Clyde McLemore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical evaluation of hypersonic forces moments and stability derivatives for combinations of flat plates, including effects of blunt leading edges, by Newtonian impact theory / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Walter B. Olstad and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Louis P. Tosti and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight study of a power-off landing technique applicable to re-entry vehicles. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Richard S. Bray, Maurice D. White, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical method for studying the lateral motion of atmosphere entry vehicles. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Robert E. Slye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of a hypersonic glider configuration at a mach number of 6 and at full-scale Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alvin Seiff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A self-adaptive missile guidance system for statistical inputs / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by H. Rodney Peery and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The design of feedback control systems containing a saturation type nonlinearity. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Stanley F. Schmidt, Eleanor V. Harper, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determining inertias by using the amplitude decay rate of a mechanical oscillating system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Gene T. Carpenter, Dan T. Meredith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gimbal geometry and attitude sensing of the ST-124 stabilized platform / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerc]e, [1962]), by Richard L. Moore, Herman E. Thomason, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Saturn vehicle attitude resolver computer error analysis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Herman E. Thomason and United States National Aeronautics and Space Administration (page images at HathiTrust)
• X-15 airplane stability augmentation system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Lawrence W. Taylor, George B. Merrick, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Richard F. Vomaske, Fred J. Drinkwater, Melvin Sadoff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A two-impulse plan for performing rendezvous on a once-a-day basis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Bird, David F. Thomas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard E. Kuhn, Kalman J. Grunwald, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of guidance sensitivity for various low-thrust transfers from Earth to Mars/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Alan L. Friedlander and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Ronald M. Gerdes and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph L. Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subsonic wind-tunnel investigation of errors indicated by total-pressure tubes in the flow field of a body simulating the nose of the X-15 research airplane. William J. Alford Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William J. Alford and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Albert L. Braslow, Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the static longitudinal aerodynamic characteristics of a 1/10-scale model of the Blue Scout Jr. at mach numbers from 0.40 to 1.03 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Thomas C. Kelly, Robert J. Keynton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Human pilots' dynamic response characteristics measured in flight and on a nonmoving simulator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Helmut A. Kuehnel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Conceptual design study of a multipurpose aerospace test facility. George C. Marshall. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by George C. Marshall and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Robert H. Kirby and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald R. McFarland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Review of the X-15 program Joseph Weil. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Joseph Weil and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of coupling between pitch and roll control inputs on the handling qualities of VTOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by John F. Garren and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Sumner A. Leadbetter, William B. Igoe, Sherman A. Clevenson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a satellite attitude control system using integrating gyros as torque sources / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John S. White and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by M. J. Queijo, G. Kimball Miller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed aerodynamic charachteristics of a cargo airplane configuration having split flaps located ahead of the wing trailing edge and leading- and trailing-edge flaps on the Canard Control. Bernard Spencer Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance evaluation of a mercury-propellant feed system for a flight-model ion engine / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Eugene V. Pawlik, Norman C. Wenger, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A theoretical investigation of the effect of cross-control derivatives on the stability characteristics of airplanes designed for flight at high mach numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Lawrence W. Brown and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1960]), by Robert E. Shanks, Charles C. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Thomas R. Turner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Charles C. Smith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a large-scale unswept wing-body-tail configuration with blowing applied over the flap and wing leading edge / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Huel Clyde McLemore, John B. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William F. Hinson, Ralph A. Falanga, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured steady-state performance of water vapor jets for use in space vehicle attitude control systems / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), by Bruce E. Tinling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Victor L. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Stuart L. Treon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gyroscopic motion of an unsymmetrical satellite under no external forces / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Manfred E. Kuebler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the longitudinal characteristics of a large-scale jet tranport model equipped with controllable thrust reversers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by David H. Hickey, Kiyoshi Aoyagi, William H. Tolhurst, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subsonic longitudinal aerodynamic characteristics of disks with elliptic cross sections and thickness-diameter rations from 0.225 to 0.425 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Fred A. Demele and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamics of a fan-in-fuselage model / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ralph L. Maki, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alan B. Kehlet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Longitudinal trim characteristics of a deflected slipstream V/Stol aircraft during level flight at transition flight speeds / Howard L. Turner and Fred J. Drinkwater III. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Howard L. Turner, Fred J. Drinkwater, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Use of conformal mapping to determine the apparent additional mass of scalloped and/or clustered cylinder configurations with experimental evaluations of results / Charles E. Watkins, Donald L. Lansing and Frederick W. Gibosn. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Charles E. Watkins, Frederick W. Gibson, Donald L. Lansing, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard Spencer, Alexander D. Hammond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-tested investigation of ailerons as a source of yaw control on the VZ-2 tilt-wing aircraft / Robert J. Pegg (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert J. Pegg and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Patrick J. Johnston, Curtis D. Snyder, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William I. Scallion and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental determination of the dynamic response of a long hydraulic line / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by John D. Regetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight examination of operating problems of V/STOL aircraft in STOL type landing and approach / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce), [1961]), by Robert C. Innis, Hervey C. Quigley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Edward C. Polhamus, Kenneth P. Spreemann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical investigation of an adaptive flight-control system using a sinusoidal test signal / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Jack E. Harris and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Angular motion of the spin axis of the Tiros I meteorological satellite due to magnetic and gravitational torques / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by W. R. Bandeen, W. P. Manger, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a model of an aerial vehicle supported by four ducted fans / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight of fifth-stage entry vehicle at mach numbers of 5 and 17 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Donn B. Kirk, Robert J. Miller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of a flow modulator using a piezoelectric crystal as the driving element. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Leon M. Wenzel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-subsonic measurements of the static stability and control and oscillatory stability derivatives of a proposed reentry vehicle having an extensible heat shield for high-heat drag / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Joseph L. Johnson, Peter C. Boisseau, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/ (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Marvin P. Fink, James L. Lastinger, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Emma Jean Landrum, K. R. Czarnecki, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by John W. Paulson, Robert E. Shanks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Byron M. Jaquet and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A fixed-base-simulator of the ability of a pilot to establish close orbits around the Moon / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by M. J. Queijo, Donald R. Riley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by John T. McShera, J. Wayne Keyes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by F. E. West and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Donald L. Loving and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic and hydrodynamic characteristics of a model of a 500,000-pound high-subsonic multijet logistics transport seaplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Walter J. Kapryan, Irving Weinstein, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of an active control system for a spinning body / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James J. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of the effects of frequency and amplitude of oscillation in sideslip on the lateral stability derivatives of a 60 degree delta wing, a 40 degree sweptback wing and an unswept wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Jacob H. Lichtenstein, James L. Williams, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of control-feel configuration on airplane longitudinal control response / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Harold L. Crane, Robert W. Sommers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by John W. Paulson, Robert E. Shanks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight investigation of an automatic gust-alleviation system in a transport airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul A. Hunter, William L. Alford, Christopher C. Kraft, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of artificial stabilization of missiles and space vehicles with exposition of four control principles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Rudolf Franz Hoelker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of the fluid oscillations in a circular cylindrical ring tank partially filled with liquid / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Helmut F. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Operational technique for transition of several types of V/STOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Fred J. Drinkwater and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Kiyoshi Aoyagi, Richard A. deSavigny, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Hervey C. Quigley, David G. Koenig, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Norman M. McFadden, Donovan R. Heinle, Richard F. Vomaske, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by T. Bradley Curry, Norman L. Crabill, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul F. Yaggy, Kenneth W. Mort, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of mass-loading variations and applied moments on motion and control of a manned rotating space vehicle. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William D. Grantham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method for obtaining the nonlinear aerodynamic stability characteristics of bodies of revolution from free-flight tests / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Donn B. Kirk and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Attitude control requirements for hovering determined through the use of a piloted flight simulator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Alan E. Faye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a mach number of 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ross B. Robinson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William C. Sleeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hovering flight investigation of two methods of controlling a man-carrying ducted-fan vehicle of the flying-platform type. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Lysle P. Parlett and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Jack F. Runckel, Gerald Hieser, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Harold L. Crane and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a solar sensor for use in space-vehicle orientation control systems. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul R. Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simulator studies of simple attitude control for spin-stabilized vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by H. D. Garner and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of thrust vector steering for rendezvous with a near-earth satellite utilizing a three-stage vehicle launched out of the satellite plane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Charles P. Llewellyn and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Method of accurately reducing the spin rate of a rotating spacecraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Henry J. Cornille and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed longitudinal characteristics of a airplane configuration including effects of canard and wing trailing-edge flap controls in combination / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Bernard Spencer, William C. Sleeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James H. Otis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Charles L. Ladson, Thomas A. Blackstock, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• VTOL height-control requirements in hovering as determined from motion simulation study / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John F. Garren, Arthur Assadourian, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Report on the research and technological problems od manned rotating spacecraft / Langley Research Ceter Staff. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Langley Research Center Staff and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles F. Whitcomb, Harry T. Norton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by M. Leroy Spearman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics at low speed of a reentry configuration having rigid retractable conical lifting surfaces. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Paul G. Fournier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Edwin C. Foudriat and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effects of engine angular momentum on an airplane's longitudinal and lateral-directional dynamic stability /, by Bernard H. Paiewonsky, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center (page images at HathiTrust)

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