The Online Books Page

Aerodynamics, aircraft

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

Filed under: Aerodynamics, aircraft

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)
Turbulent skin-friction and heat-transfer coefficients for an inclined flat plate at high hypersonic speeds in terms of free-stream flow properties. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by James F. Schmidt and United States National Aeronautics and Space Administration (page images at HathiTrust)
Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Mary W. Jackson, K. R. Czatnecki, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Paul G. Fournier, B. Ann Bell, 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)
Review of basic principles of V/STOL aerodynamics / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard E. Kuhn and United States National Aeronautics and Space Administration (page images at HathiTrust)
Considerations of methods of improving helicopter efficiency / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Richard C. Dingeldein 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)
Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert T. Swann, Jerry C. South, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by James P. Shivers 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)
The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Travis H. Slocumb, Earl H. Andrews, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Jack F. Runckel and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William J. Monta, K. R. Czarnecki, Paul W. Howard, 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)
Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures from 1,295 degrees F to 2,910 degrees F / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Bernard Rashis 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)
Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or 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, Gene P. Menees, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of shock impingement on the distribution of heat-transfer coefficients on a right circular cylinder at mach numbers of 2.65, 3.51, and 4.44 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Robert A. Newlander 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)
External-drag estimation for slender conical ducted bodies at high mach numbers and zero angle of attack. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by E. Floyd Valentine 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)
Wind-tunnel investigation of tail buffet at subsonic and transonic speeds employing a dynamic elastic aircraft model / Robert N. Rigby and Elden S. Cornette. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert N. Rigby, Elden S. Cornette, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigating of the drag and static stability characteristics of four helicopter fuselage models / George E. Sweet and Julian L. Jenkins Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by George E. Sweet, Julian L. Jenkins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A Wind-tunnel investigation of the longitudinal aerodynamic charachteristics of two full-scale helicopter fuselage models with appendages / Julian L. Jenkins, Matthew M. Winston and George E. Sweet. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Julian L. Jenkins, George E. Sweet, Matthew M. Winston, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Longitudinal stability and control of a tilt-wing VTOL aircraft model with rigid and flapping propeller blades / Louis P. Tosti. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Louis P. Tosti 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)
Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Kalman J. Grunwald, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gary T. Chapman 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)
Recovery temperature transition and heat-transfer measurements at mach 5 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul F. Brinich and United States National Aeronautics and Space Administration (page images at HathiTrust)
Measured surface defects on typical transonic airplanes and analysis of their drag contribution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Elmer A. Horton, Neal Tetervin, 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)
Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Peter C. Boisseau and United States National Aeronautics and Space Administration (page images at HathiTrust)
Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Gerald L. Hunt, Gerald D. Walberg, 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)
Estimate of shock standoff distance ahead of a general stagnation point / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Eli Reshotko 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)
Nomographic solution of the mometum equation for VTOL-STOL aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Harry H. Heyson 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)
Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Arthur Henderson, Dorothy O. Braswell, 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)
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)
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)
Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Edwin J. Saltzman 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)
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)
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)
An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Donald E. Gault and United States National Aeronautics and Space Administration (page images at HathiTrust)
Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Hervey C. Quigley and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Frederick W. Boltz, Clyde Q. Allen, George C. Kenyon, 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)
Exploratory study of the reduction in friction drag due to streamwise injection of helium. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Byron L. Swenson and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental determination of the pressure distribution on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Henry C. Lessing, Gene P. Menees, John L. Troutman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Shock-wave patterns on a cranked-wing configuration / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Robert I. Sammonds and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transition Reynolds numbers of separated flows at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Howard K. Larson, Stephen J. Keating, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Large-scale wind-tunnel tests and evaluation of the low-speed performance of a 35 degree sweptback wing jet transport model equipped with a blowing boundary-layer-control flap and leading edge slat / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by David H. Hickey, Kiyoshi Aoyagi, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A correlation study of the bow wave profiles of blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962 ]), by Alvin Seiff, Ellis E. Whiting, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Longitudinal force and moment data at mach numbers from 0.60 to 1.40 for a family of elliptic cones with various semiapex angles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Louis S. Stivers, Lionel L. Levy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Flight-determined aerodynamic-noise environment of an airplane nose cone up to a Mach number of 2 (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Norman J. McLeod 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)
Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert L. Nelson, Clement J. Welsh, 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 method for calculating the generalized aerodynamic forces on rectangular wings deforming symmetrically in supersonic flight with indicial or sinusoidal time dependence / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Rueben Bond 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)
Heat transfer to 0 degree and 75 degree swept blunt leading edges in free flight at mach numbers from 1.90 to 3.07. Robert L. O'Neal and Aleck C. Bond. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert L. O'Neal, Aleck C. Bond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Division of aerodynamic loads on a semispan tilting-ducted-propeller model in hovering and transition flight. : Kalman J. Grunwald and Kenneth W. Goodson. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Kalman J. Grunwald, Kenneth W. Goodson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Charles J. Shoemaker, John R. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1962), by P. Calvin Stainback 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)
Stability of three-dimensional compressible boundary layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Eli Reshotko and United States National Aeronautics and Space Administration (page images at HathiTrust)
Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Donald L. Lansing 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)
Effects of forebody length on the stability and control characteristics at a Mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by M. Leroy Spearman, Cornelius Driver, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Pressure distributions at Mach number 2.05 on a series of highly swept arrow wings employing various degrees of twist and camber / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harry W. Carlson 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)
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)
An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Thomas C. O'Bryan 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)
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)
Heat transfer at the reattachment zone of separated laminar boundary layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Paul M. Chung and United States National Aeronautics and Space Administration (page images at HathiTrust)
Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Gary T. Chapman 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)
Measurements of flow duration in a low-pressure shock tube / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Virgil A. Sandborn 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)
Sound pressures and correlations of noise on the fuselage of a jet aircraft in flight / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Russell D. Shattuck and United States National Aeronautics and Space Administration (page images at HathiTrust)
The blunt plate in hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Donald L. Baradell, Mitchel H. Bertram, 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)
A Wind-tunnel investigation of pressure fluctuations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane / John W. McKee and Thomas A. Byrdsong. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John W. McKee, Thomas A. Byrdsong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of multiple-nozzle geometry on jet noise generation. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Vern G. Rollin 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)
Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by K. R. Czarnecki, William J. Monta, 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)
A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location / (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)
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)
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)
Aerodynamic heating and boundary-layer transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 X 10(6) / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Benjamine J. Garland, Katherine C. Speegle, Andrew G. Swanson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harold Ferguson, John W. Schaefer, 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)
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)
Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including 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 Kalman J. Grunwald 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)
Comparison of experimental and numerical results for the flow of a perfect gas about blunt-nosed bodies / Mamoru Inouye and Harvard Lomax. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Mamoru Inouye, Harvard Lomax, 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)
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)
Free-flight investigation of radio-controlled models with parawings / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Donald E. Hewes 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 interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model / (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)
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)
Wind-tunnel tests of two full-scale helicopter fuselages (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by James C. Biggers 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)
Ground and in-flight acoustic and performance characteristics of jet-aircraft exhaust noise supressors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Willard D. Coles, William H. Swann, John A Mihaloew, 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)
Hovering measurements for twin-rotor configurations with and without overlap / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by George E. Sweet and United States National Aeronautics and Space Administration (page images at HathiTrust)
Damage incurred on a tilt-wing multi-propeller VTOL/STOL aircraft operating over a level, gravel-covered surface / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Robert J. Pegg and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of base bleed and terminal fairings on the performance of exhaust-nozzle-afterbody combinations at mach numbers of 1.93, 2.55 and 3.05 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Harry T. Norton, Arvid L. Keith, 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)
Heat-transfer measurements at a mach number of 4.95 on two 60 degree sweot delta wings with blunt leading edges and dihedral angles of 0 degrees and 46 degrees / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by P. Calvin Stainback and United States National Aeronautics and Space Administration (page images at HathiTrust)
A note on the drag due to lift of delta wings at mach numbers up to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Robert S. Osborne, Thomas C. Kelly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Elden S. Cornette 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)
Some simple solutions to the problem of predicting boundary-layer self-induced pressures / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Michael H. Bertram, Thomas A. Blackstock, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by K. R. Czarnecki 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)
Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Frederick W. Boltz and United States National Aeronautics and Space Administration (page images at HathiTrust)
A method of determining aerodynamic-influence coefficients from wind-tunnel data for wings at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Patrick A. Gainer and United States National Aeronautics and Space Administration (page images at HathiTrust)
Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100⁰ total-angle cone and a 10⁰ half-angle conical flare section up to a mach number of 4.08 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Bernard Rashis, Aleck C. Bond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Franklyn B. Fuller 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)
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)
A study of laminar compressible viscous pipe flow accelerated by an axial body force, with application to magnetogasdynamics. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by E. Dale Martin and United States National Aeronautics and Space Administration (page images at HathiTrust)
Constant density approximations for the flow behind axisymmetric shock waves. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Albert G. Munson and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effects of boattailing and nozzle extension on the thrust-minus-drag of a multiple-jet configuration. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by William R. Scott and United States National Aeronautics and Space Administration (page images at HathiTrust)
Measurements of aerodynamic heat transfer and boundary-layer transition on a 15⁰ cone in free flight at supersonic mach numbers up to 5.2 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles B. Rumsey, Dorothy B. Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transonic and supersonic wind-tunnel tests of wing-body combinations designed for high efficiency at a mach number of 1.41 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Frederick C. Grant, John R. Sevier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for a reflex cambered wing and a cambered and twisted wing having the same swept planform / (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)
A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes / (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)
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)
The lower bound of attainable sonic-boom overpressure and design methods of approaching this limit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Harry W. Carlson 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)
Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Charles R. Rumsey, Dorothy B. Lee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), by Ivan E. Beckwith and United States National Aeronautics and Space Administration (page images at HathiTrust)
An exploratory study of a parawing as a high-lift device for aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Rodger L. Naeseth and United States National Aeronautics and Space Administration (page images at HathiTrust)

More items available under narrower terms.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.