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Primary view of Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Burrows, Dale L.
June 17, 1954
Primary view of Distribution of losses behind a compressor rotor as measured by a rotating rake
Godwin, William R.
January 17, 1956
Primary view of An experimental study of a method for designing fuselage side air inlets for high performance at transonic and low supersonic speeds
Howell, Robert R. & Trescot, Charles D., Jr.
January 17, 1955
Primary view of Effect of large negative dihedral of the horizontal tail on longitudinal and lateral stability characteristics of a swept-wing configuration at transonic speeds
Arabian, Donald D.
January 17, 1956
Primary view of Comparison of Performance and Component Frontal Areas of Hypothetical Two-Spool and One-Spool Turbojet Engines
Dugan, James F., Jr.
January 17, 1956
Primary view of Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude
Mallett, William E. & Groesbeck, Donald E.
January 17, 1956
Primary view of Some interference effects that influence vertical-tail loads at supersonic speeds
Edwards, S. Sherman
February 17, 1956
Primary view of Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle Upon the Pressure of the Base Annulus of a Body of Revolution
Bromm, August F., Jr. & O'Donnell, Robert M.
December 17, 1954
Primary view of The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane
Abramovitz, Marvin & Van Dyke, Rudolph D., Jr.
December 17, 1954
Primary view of An Investigation of the Effects of Jet Exhaust and Reynolds Number Upon the Flow Over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
Grigsby, Carl E.
June 17, 1954
Primary view of Thrust and pumping characteristics of a series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds
Hearth, Donald P. & Valerino, Alfred S.
November 17, 1954
Primary view of Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces
Hikido, Katsumi; Hayashi, Paul H. & Lessing, Henry C.
May 17, 1956
Primary view of Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96
Hadaway, William M.
February 17, 1956
Primary view of Wind-tunnel investigation of horizontal tails 3: unswept and 35 degrees swept-back plan forms of aspect ratio 6
Dods, Jules B., Jr.
December 17, 1948
Primary view of Free-Flight Investigation of the Rolling Effectiveness of a Wing-Spoiler Arrangement at High Subsonic, Transonic, and Supersonic Speeds
Sandahl, Carl A.
May 17, 1948
Primary view of Ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
Hall, Charles F. & Frank, Joseph L.
November 17, 1948
Primary view of Control requirements and control parameters for a ram jet with variable-area exhaust nozzle
Boksenbom, Aaron S. & Novik, David
November 17, 1948
Primary view of Qualitative Measurements of Relative Flap Effectiveness at Transonic Speeds on a Series of Five Thin Airfoils With 25-Percent-Chord Flaps and Various Amounts of Sweepback
Crane, Harold L. & McLaughlin, Milton D.
May 17, 1948
Primary view of Theoretical Investigation of the Stability at Negative Static Margins of a Supersonic Missile With an Autopilot Sensitive to Pitch Angle and Pitching Velocity
Cole, Henry A., Jr. & Abramovitz, Marvin
March 17, 1952
Primary view of Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Rom, F. E. & Wachtl, W. W.
December 17, 1952
Primary view of Investigation of Turbines for Driving Supersonic Compressors: 1: Design and Performance of First Configuration
Stewart, Warner L.; Schum, Harold J. & Whitney, Warren J.
June 17, 1952
Primary view of Effects of wing elasticity on the aerodynamic characteristics of a 45 degree sweptback-wing-fuselage combination measured in the Langley 8-foot transonic tunnel
Osborne, Robert S. & Mugler, John P., Jr.
September 17, 1952
Primary view of Investigation at high and low subsonic Mach numbers of two symmetrical 6-percent-thick airfoil sections designed to have high maximum lift coefficients at low speeds
Paradiso, Nicholas J.
October 17, 1952
Primary view of Investigation of ram-jet afterburning as a means of varying effective exhaust nozzle area
Perchonok, Eugene & Wilcox, Fred A.
November 17, 1952
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