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Primary view of Effect of Inlet-Guide-Vane Angle on Blade Vibration and Rotating Stall of 13-Stage Axial-Flow Compressor in Turbojet Engine
Calvert, Howard F.; Medeiros, Arthur A. & Johnson, Donald F.
May 22, 1956
Primary view of Flight investigation of pentaborane fuel in 9.75-inch-diameter ram-jet engine with downstream fuel injection
Disher, John H. & Jones, Merle L.
April 22, 1957
Primary view of Investigation of High-Temperature Operation of Liquid-Cooled Gas Turbines 1: Turbine Wheel of Aluminum Alloy, a High-Conductivity Nonstrategic Material
Kottas, Harry & Sheflin, Bob W.
July 22, 1948
Primary view of Effect of Inlet-Air Parameters on Combustion Limit and Flame Length in 8-Inch-Diameter Ram-Jet Combustion Chamber
Cervenka, A. J. & Miller, R. C.
July 22, 1948
Primary view of Longitudinal Stability Characteristics of a 42 Degree Sweptback Wing and Tail Combination at a Reynolds Number of 6.8 X 10 (Exp 6)
Spooner, Stanley H. & Martina, Albert P.
July 22, 1948
Primary view of Evaluation of Gust and Draft Velocities From Flights of an AT-6 Airplane Within Cumulus Clouds July 1, 1947 to July 22, 1947 at Clinton County Army Air Field, Ohio
Funk, Jack
March 22, 1948
Primary view of Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 3: inlet enclosing 37.2 percent of the maximum circumference of the forebody
Davis, Wallace F. & Edwards, Sherman S.
July 22, 1948
Primary view of Stability Results Obtained With Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89
Barlow, William H. & Lilly, Howard C.
April 22, 1949
Primary view of Notes on the Application of Airfoil Studies to Helicopter Rotor Design
Gustafson, F. B.
September 22, 1948
Primary view of Tank spray tests of a jet-powered model fitted with NACA hydro-skis
Wadlin, Kenneth L. & Ramsen, John A.
July 22, 1948
Primary view of Experimental data concerning the effect of high heat-input rates on the pressure drop through radiator tubes
Habel, Louis W. & Gallagher, James J.
September 22, 1948
Primary view of Effects of stabilizing fins and a rear-support sting on the base pressure of a body of revolution in free flight at Mach numbers from 0.7 to 1.3
Hart, Roger G.
September 22, 1952
Primary view of Preliminary air-flow and thrust calibrations of several conical Cooling-air ejectors with a primary to secondary temperature ratio of 1.0 I :diameter ratios of 1.21 and 1.10
Greathouse, W. K. & Hollister, D. P.
July 22, 1952
Primary view of Effect of water vapor on combustion of magnesium hydrocarbon slurry fuels in small-scale afterburner
Tower, Leonard K.
October 22, 1952
Primary view of Some Effects of Spanwise Aileron Location and Wing Structural Rigidity on the Rolling Effectiveness of 0.3-Chord Flap-Type Ailerons on a Tapered Wing Having 63 Degrees Sweepback at the Leading Edge and Naca 64A005 Airfoil Sections
Strass, H. Kurt; Fields, E. M. & Schult, Eugene D.
June 22, 1951
Primary view of Effects of Reynolds Number on the Aerodynamic Characteristics of a Delta Wing at Mach Number of 2.41
Hatch, John E., Jr. & Hargrave, L. Keith
October 22, 1951
Primary view of Investigation of the Effects of Variations in the Reynolds Number Between 0.4 X 10(Exp 6) 3.0 X 10(Exp 6) on the Low-Speed Aerodynamic Characteristics of Three Low-Aspect-Ratio Symmetrical Wings With Rectangular Plan Forms
Jones, George W., Jr.
September 22, 1952
Primary view of Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds
Gillis, Clarence L. & Chapman, Rowe, Jr.
January 22, 1953
Primary view of Investigation of Turbines for Driving Supersonic Compressors 2: Performance of First Configuration With 2.2 Percent Reduction in Nozzle Flow Area
Stewart, Warner L.; Schum, Harold J. & Wong, Robert Y.
July 22, 1952
Primary view of Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds
Boyd, John W.
July 22, 1952
Primary view of Effects of Some Primary Variables of Rectangular Vortex Generators on the Static-Pressure Rise Through a Short Diffuser
Valentine, E. Floyd & Carroll, Raymond B.
May 22, 1952
Primary view of Some Wind-Tunnel Results of an Investigation of the Flutter of Sweptback- and Triangular-Wing Models at Mach Number 1.3
Tuovila, W. J.
May 22, 1952
Primary view of Method of Estimating the Stick-Fixed Longitudinal Stability of Wing-Fuselage Configurations Having Unswept or Swept Wings
McLaughlin, Milton D.
January 22, 1952
Primary view of Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section
Dugan, Duane W.
July 22, 1952
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