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Primary view of Equation of State and Heat Content of Uranium
Brout, Robert H.
February 20, 1957
Primary view of Nature of atmospheric dust. Progress report to January 15, 1955
Heininger, C. & Turkevich, J.
January 20, 1955
Primary view of Thermal Bowing of Core Subassemblies
De Stordeur, Arnold
February 20, 1959
Primary view of Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane
Fisher, Lloyd J. & Morris, Garland J.
April 20, 1950
Primary view of Investigation of the Effects of Leading-Edge Flaps on the Aerodynamic Characteristics in Pitch at Mach Numbers From 0.40 to 0.93 of a Wing-Fuselage Configuration With a 45 Degree Sweptback Wing of Aspect Ratio 4
Spreemann, Kenneth P. & Alford, William J., Jr.
August 20, 1953
Primary view of Friction and surface damage of several corrosion-resistant materials
Peterson, Marshall B. & Johnson, Robert L.
February 20, 1952
Primary view of An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc section and 40 degree sweepback: a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.40
Smith, Norman F.; Kainer, Julian H. & Webster, Robert A.
April 20, 1951
Primary view of Flight Investigation From Mach Number 0.8 to 2.0 to Determine Some Effects of Wing-to-Tail Distance on the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing-Canard Missile
Brown, Clarence A., Jr. & Lundstrom, Reginald R.
June 20, 1952
Primary view of Skin-friction drag and boundary-layer transition on a parabolic body of revolution (NACA RM-10)at a Mach number of 1.6 in the Langley 4-by-4 foot supersonic pressure tunnel
Czarnecki, K. R. & Marte, Jack E.
May 20, 1952
Primary view of Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54
Wallskog, Harvey A. & Morrow, John D.
April 20, 1953
Primary view of Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range From 0.5 to 0.95
Baker, Thomas F.
November 20, 1953
Primary view of Analysis of performance of four symmetrical-diagram-type subsonic inlet-stage axial-flow compressors
Jackson, Robert J.
January 20, 1954
Primary view of Wind-Tunnel Investigation of the Effects of a Fence and a Leading-Edge Notch on the Aerodynamic Loading Characteristics in Pitch of a 45 Degree Sweptback Wing at High Subsonic Speeds
Kuhn, Richard E.; Wiggins, James W. & Byrnes, Andrew L., Jr.
October 20, 1953
Primary view of Performance of a supersonic mixed-flow rotor with a swept leading edge and 0.52 inlet radius ratio
Goldstein, Arthur W. & Schacht, Ralph L.
November 20, 1953
Primary view of Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
Stivers, Louis S., Jr.; Walker, Harold J. & Beard, Luther, Jr.
April 20, 1951
Primary view of Review of Current and Anticipated Lubricant Problems in Turbojet Engines
unknown creator
April 20, 1951
Primary view of Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids
Jackson, Joseph L.
December 20, 1950
Primary view of Tabulated pressure coefficients and aerodynamic characteristics measured on the wing of the Bell X-1 airplane in an unaccelerated low-speed stall, in push-overs at Mach numbers of 0.83 and 0.99, and in a pull-up at a Mach number of 1.16
Knapp, Ronald J.
September 20, 1951
Primary view of Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the D-558-I Research Airplane Through a Mach Number Range of 0.80 to 0.89 and Throughout the Normal-Force-Coefficient Range at Mach Numbers of 0.61, 0.70, 0.855, and 0.88
Keener, Earl R. & Bandish, Rozalia M.
August 20, 1951
Primary view of Effective Modulus in Plastic Buckling of High-Strength Aluminum-Alloy Sheet
Miller, James A. & Jacobs, Pearl V.
September 20, 1951
Primary view of Experimental Investigation of Forced-Convection Heat-Transfer Characteristics of Lead-Bismuth Eutectic
Lubarsky, Bernard
September 20, 1951
Primary view of An Investigation at Transonic Speeds of the Effects of Control Chord and Span on the Control Characteristics of a Tapered Wedge-Type Wing of Aspect Ratio 2.5: Transonic-Bump Method
Vogler, Raymond D.; Lockwood, Vernard E. & Turner, Thomas R.
September 20, 1951
Primary view of Experimental Investigation of Effect of Jet Exit Configuration on Thrust and Drag
Callaghan, Edmund E. & Coles, Willard D.
December 20, 1951
Primary view of The Effect on Zero-Lift Drag of an Indented Fuselage or a Thickened Wing-Root Modification to a 45 Degree Sweptback Wing-Body Configuration as Determined by Flight Tests at Transonic Speeds
Pepper, William B.
September 20, 1951
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