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Primary view of High Altitude Performance Investigation of J65-B-3 Turbojet Engine With Both JP-4 and Gaseous Hydrogen Fuels
Kaufman, Harold R.
April 2, 1957
Primary view of Investigation of Flutter Characteristics of Three Low-Aspect-Ratio All-Movable Half-Span Control Surfaces at Mach Numbers From 1.49 to 2.87
Morgan, Homer G.; Figge, Irving E. & Presnell, John G., Jr.
May 2, 1958
Primary view of Some Effects of Aeroelasticity on the Rolling Effectiveness of a 10-Percent-Scale Model of the Mcdonnell F-101A Airplane Wing at Mach Numbers From 0.5 to 1.2
English, Roland D.
September 2, 1955
Primary view of Effects of Modifications to a Control Surface on a 6-Percent-Thick Unswept Wing on the Transonic Control-Surface Flutter Derivatives
Wyss, John A.; Sorenson, Robert M. & Gambucci, Bruno J.
May 2, 1958
Primary view of NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations
von Glahn, Uwe; Callaghan, Edmund E. & Gray, Vernon H.
May 2, 1951
Primary view of Large-Scale Wind-Tunnel Tests of an Airplane Model With a 45 Degree Sweptback Wing of Aspect Ratio 2.8 With Area Suction Applied to Trailing-Edge Flaps and With Several Wing Leading-Edge Modifications
Koenig, David G. & Aoyagi, Kiyoshi
November 2, 1956
Primary view of Tests With Hydrogen Fuel in a Simulated Afterburner
Kerslake, W. R. & Dangle, E. E.
July 2, 1956
Primary view of Organophosphorus Compounds in Rocket-Engine Applications
Ladanyi, Dezso J. & Hennings, Glen
April 2, 1954
Primary view of Some Research on the Lift and Stability of Wing-Body Combinations
Purser, Paul E. & Fields, E. M.
July 2, 1959
Primary view of Performance of a Short Turbojet Combustor With Hydrogen Fuel in a Quarter-Annulus Duct and Comparison With Performance in a Full-Scale Engine
Friedman, Robert; Norgren, Carl T. & Jones, Robert E.
July 2, 1956
Primary view of Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers
Ulmann, Edward F. & Bertram, Mitchel H.
November 2, 1953
Primary view of Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 3: Methods for Determining Power and Efficiency
Ellerbrock, Herman H., Jr. & Ziemer, Robert R.
August 2, 1950
Primary view of Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic bump method
Vogler, Raymond D.
March 2, 1950
Primary view of Preliminary analysis of effects of air cooling turbine blades on turbojet-engine performance
Schramm, Wilson B.; Nachtigall, Alfred J. & Arne, Vernon L.
August 2, 1950
Primary view of Effects of boundary-layer control on the longitudinal characteristics of a 45 degrees swept-forward wing-fuselage combination
McCormack, Gerald M. & Cook, Woodrow L.
February 2, 1950
Primary view of Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body
Stivers, Louis S. & Malick, Alexander W.
February 2, 1950
Primary view of Some properties of beryllium oxide and beryllium oxide - columbium ceramals
Robards, C. F. & Gangler, J. J.
March 2, 1951
Primary view of Correlation of forced-convection heat-transfer data for air flowing in smooth platinum tube with long-approach entrance at high surface and inlet-air temperatures
Desmon, Leland G. & Sams, Eldon W.
November 2, 1950
Primary view of Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap
Czarnecki, K. R. & Mueller, James N.
January 2, 1951
Primary view of An investigation of convergent-divergent diffusers at Mach number 1.85
Wyatt, DeMarquis D. & Hunczak, Henry R.
February 2, 1951
Primary view of Experimental investigation of effects of design changes on performance of large-capacity centrifugal compressors
Withee, Joseph R., Jr.; Kovach, Karl & Ginsburg, Ambrose
March 2, 1951
Primary view of Altitude Operation of Gas-Turbine Engine With Variable-Area Fuel-Nozzle System
Gold, H. & Rosenzweig, S.
April 2, 1951
Primary view of Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 4 with NACA 0005-63 section
Heitmeyer, John C. & Stephenson, Jack D.
February 2, 1951
Primary view of Flight Investigation of the Effect of Thickening the Aileron Trailing Edge on Control Effectiveness for Sweptback Tapered Wings Having Sharp-and Round-Nose Sections
Strass, H. Kurt & Fields, Edison M.
May 2, 1950
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