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Primary view of Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Martz, C. William & Goslee, John W.
October 30, 1953
Primary view of A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees
Cooper, Morton; Gapcynski, John P. & Hasel, Lowell E.
October 30, 1952
Primary view of Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
Robinson, Glenn H.; Cothren, George E., Jr. & Pembo, Chris
March 30, 1955
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Removal of secondary-flow accumulations in a two-dimensional turbine nozzle passage by boundary-layer bleed
Wong, Robert Y.
June 30, 1955
Primary view of Design considerations of a condensing system for vaporized magnesium
Witzke, Walter R.; Prok, George M. & Keller, Thomas A.
November 30, 1955
Primary view of Effects of Canopy, Revised Vertical Tail, and a Yaw-Damper Vane on the Aerodynamic Characteristics of a 1/16-Scale Model of the Douglas D-558-II Research Airplane at a Mach Number of 2.01
Robinson, Ross B.
August 30, 1954
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a 1/15-Scale Model of the Grumman F11F-1F Airplane at Mach Numbers of 1.56, 1.76, 2.06, and 2.53
Turner, Kenneth L. & Fournier, Roger H.
November 30, 1956
Primary view of A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
Phelps, E. Ray & Boyd, John W.
April 30, 1957
Primary view of Wind-Tunnel Investigation at High Subsonic Speeds of the Effects on Static Stability Characteristics of Various Modifications to a Swept-Wing Fighter-Type Airplane Model
Goodson, Kenneth W.
April 30, 1957
Primary view of Experimental and theoretical investigation of rotating-stall characteristics of single-stage axial-flow compressor with hub-tip ratio of 0.76
Graham, Robert W. & Prian, Vasily D.
November 30, 1953
Primary view of Tabulated pressure data for a series of controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01
Lord, Douglas R. & Czarnecki, K. R.
March 30, 1956
Primary view of Experimental Investigation of a 0.4 Hub-Tip Diameter Ratio Axial-Flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers 3: Effect of Tip Taper on Over-All and Blade-Element Performances
Montgomery, John C. & Glaser, Frederick
March 30, 1956
Primary view of Altitude performance evaluation of J71-A-11 turbojet engine
Useller, James W. & Pappas, George E.
March 30, 1956
Primary view of Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60
Robins, A. Warner
October 30, 1953
Primary view of Experimental Investigation at High Subsonic Speeds of the Rolling-Stability Derivatives of a 1/22 Scale Model of the Republic F-105 Airplane
Sleeman, William C., Jr. & Hayes, William C., Jr.
June 30, 1955
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Investigation of the Static Stability Characteristics of Five Hypersonic Missile Configurations at Mach Numbers From 2.29 to 4.65
Turner, Kenneth L. & Appich, W. H., Jr.
June 30, 1958
Primary view of Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration With a Low-Aspect-Ratio Wing and Blunt Nose at Mach Numbers From 1.2 to 2.1
Brown, Clarence A., Jr.
September 30, 1957
Primary view of Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine: 1: Rotor Blades With 10 Tubes in Cooling-Air Passages
Ellerbrock, Herman H., Jr. & Stepka, Francis S.
July 30, 1950
Primary view of Preliminary Performance Data Obtained in a Full-Scale Free-Jet Investigation of a Side-Inlet Supersonic Diffuser
Farley, John M. & Smith, Ivan D.
November 30, 1954
Primary view of Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water With Variable Fluid Properties in a Smooth Tube
Deissler, R. G. & Taylor, M. F.
January 30, 1953
Primary view of Experimental and Theoretical Determination of Forces and Moments on a Store and on a Store- Pylon Combination Mounted on a 45 Degree Swept- Wing-Fuselage Configuration at a Mach Number of 1.61
Morris, Odell A.; Carlson, Harry W. & Geier, Douglas J.
January 30, 1958
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