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Primary view of Wind-Tunnel Investigation at Low Speed of Sideslipping, Rolling, Yawing, and Pitching Characteristics for a Model of a 45 Degree Swept-Wing Fighter-Type Airplane
Jaquet, Byron M. & Fletcher, H. S.
September 1, 1955
Primary view of Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages 6: over-all performance, rotating stall, and blade vibration at low and intermediate compressor speeds
Standahar, Raymond M.; Hanson, Morgan P. & Geye, Richard P.
November 1, 1955
Primary view of Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Complete Model With an Unswept Wing and a Sweptback Horizontal Tail at Two Vertical Locations
Hieser, Gerald & Kudlacik, Louis
September 1, 1955
Primary view of Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory
Swett, Clyde C., Jr.
November 1, 1955
Primary view of Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips
Weinflash, Bernard
September 1, 1955
Primary view of Comparative Dispersion Data From Ground-Launched 2.25-Inch Rockets Equipped With Cruciform and Monoplane Fins
Purser, Paul E.
November 1, 1955
Primary view of Effect of Reduced Stator-Blade Trailing-Edge Thickness on Over-All Performance of a Transonic Turbine
Whitney, Warren J.; Stewart, Warner L. & Wong, Robert Y.
November 1, 1955
Primary view of Pressure recovery at supersonic speeds through annular duct inlets situated in a region of appreciable boundary layer 1: addition of energy to the boundary layer
Davis, Wallace F. & Brajnikoff, George B.
April 1, 1948
Primary view of Investigation of Flow Conditions and the Nature of the Wall-Constriction Effect Near and at Choking by Means of the Hydraulic Analogy
Matthews, Clarence W. & Wright, Ray H.
September 1, 1948
Primary view of Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
Solomon, William
October 1, 1948
Primary view of Analysis of V-g records from the Grumman F8F-2 airplane
Thornton, James O.
July 1, 1952
Primary view of The Vertical-Tail Loads Measured During a Flight Investigation on a Jet-Powered Bomber Airplane
Cooney, T. V.
May 1, 1953
Primary view of An Investigation at Transonic Speeds of the Aerodynamic Characteristics of an Air Inlet Installed in the Root of a 45 Degree Sweptback Wing
Howell, Robert R. & Keith, Arvid L., Jr.
October 1, 1952
Primary view of Stability and Control Flight Tests of a 0.13-Scale Model of the Consolidated-Vultee XFY-1 Airplane in Take-Offs, Landings, and Hovering Flight: TED No. NACA DE 368
Lovell, Powell M., Jr.; Smith, Charles C., Jr. & Kirby, Robert H.
October 1, 1952
Primary view of Some effects of body cross-sectional shape, including sunken-canopy design, on drag as shown by rocket-powered-model tests at Mach numbers from 0.8 to 1.5
Stoney, William E., Jr. & Putland, Leonard W.
July 1, 1952
Primary view of Preliminary investigation of the altitude performance of pentaborane and a pentaborane : JP-4 blend in an experimental 9.5-inch-diameter tubular combustor
Kaufman, Warner B. & Branstetter, J. Robert
April 1, 1957
Primary view of Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: Aspect-ratio series
Kuhn, Richard E. & Wiggins, James W.
April 1, 1952
Primary view of Thermal shock resistance and high-temperature strength of a molybdenum disilicide - aluminum oxide ceramic
Maxwell, W. A. & Smith, R. W.
October 1, 1953
Primary view of Horizontal-Tail Load Measurements at Transonic Speeds of the Bell X-1 Research Airplane
Rogers, John T.
September 1, 1953
Primary view of Some Experimental Effects of Afterbody Shape on the Zero-Lift Drag of Bodies for Mach Numbers Between 0.8 and 1.3
Stoney, William E., Jr.
October 1, 1953
Primary view of Downwash Behind a Triangular Wing of Aspect Ratio 3 - Transonic Bump Method
Axelson, John A.
December 1, 1953
Primary view of Investigation of the Low-Speed Aerodynamic Characteristics of a Variable-Sweep Airplane Model With a Twisted and Cambered Wing
Kemp, William B., Jr.; Becht, Robert E. & Few, Albert G., Jr.
February 1, 1952
Primary view of Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the static lateral stability characteristics at M = 2.01
Hamilton, Clyde V.
August 1, 1952
Primary view of Considerations in the adaptation of low-cost fuels to gas-turbine-powered commercial aircraft
Barnett, Henry C. & McCafferty, Richard J.
October 1, 1953
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