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Primary view of Effect of Ice Formations on Section Drag of Swept NACA 63A-009 Airfoil with Partial-Span Leading-Edge Slat for Various Modes of Thermal Ice Protection
von Glahn, Uwe H. & Gray, Vernon H.
March 15, 1954
Primary view of Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine
McKann, Robert E. & Petynia, William W.
April 15, 1954
Primary view of Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models
Church, James D.
July 15, 1954
Primary view of Investigation of Adjustable Supersonic Inlet in Combination With J34 Engine Up to Mach 2.0
Nettles, J. C. & Leissler, L. A.
October 15, 1954
Primary view of Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature
Donoughe, Patrick L. & Livingood, John N. B.
July 15, 1954
Primary view of Similar Solutions for the Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient
Cohen, Clarence B. & Reshotko, Eli
October 15, 1954
Primary view of Performance and Boundary-Layer Data From 12 Degree and 23 Degree Conical Diffusers of Area Ratio 2.0 at Mach Numbers Up to Choking and Reynolds Numbers Up to 7.5 X 10(6)
Little, B. H., Jr. & Wilbur, Stafford W.
November 15, 1954
Primary view of Effect on Drag of Longitudinal Positioning of Half-Submerged and Pylon-Mounted Douglas Aircraft Stores on a Fuselage with and without Cavities between Mach Numbers 0.9 and 1.8
Hoffman, Sherwood & Wolff, Austin L.
July 15, 1954
Primary view of Effects of angle of attack and airfoil profile on the two-dimensional flutter derivatives for airfoils oscillating in pitch at high subsonic speeds
Wyss, John A. & Herrera, Raymond
October 15, 1954
Primary view of Sea-level static equilibrium performance of actual two-spool turbojet engine and comparison with hypothetical engine
Dugan, James F., Jr.; Jansen, Emmert T.; Rohlik, Harold E. & Mallett, William E.
September 15, 1954
Primary view of A Transonic Wind-Tunnel Investigation of the Longitudinal Force and Moment Characteristics of a Plane and a Cambered 3-Percent-Thick Delta Wing of Aspect Ratio 3 on a Slender Body
Burrows, Dale L. & Palmer, William E.
November 15, 1954
Primary view of Analytical Study of the Effect of Center-of-Gravity Position on the Response to Longitudinal Control in Landing Approaches of a Swept-Wing Airplane of Low Aspect Ratio Having No Horizontal Tail
Stone, Ralph W., Jr.
October 15, 1954
Primary view of The Effect of an Operating Propeller on the Aerodynamic Characteristics at High Subsonic Speeds of a Model of a Vertical-Rising Airplane Having an Unswept Wing of Aspect Ratio 3
Sutton, Fred B. & Buell, Donald A.
November 15, 1954
Primary view of Effect of Ice Formations on Section Drag of Swept NACA 63A-009 Airfoil With Partical-Span Leading-Edge Slat for Various Modes of Thermal Ice Protection
von Glahn, Uwe H. & Gray, Vernon H.
March 15, 1954
Primary view of Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet
Miller, Robert R. & Bloomer, Harry E.
June 15, 1954
Primary view of Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness
Heitmeyer, John C.
March 15, 1954
Primary view of Investigation of a missile airframe with control surfaces consisting of projecting quadrants of the nose cone
Lazzeroni, Frank A.
March 15, 1954
Primary view of Altitude performance of compressor, turbine, and combustor components of 600-B9 turbojet engine
Prince, William R. & Wile, Dorwin B.
March 15, 1954
Primary view of Investigation of a 10-Stage Subsonic Axial-Flow Research Compressor 5: Effect of Reducing Inlet-Guide-Vane Turning on Over-All and Inlet-Stage Performance
Budinger, Ray E. & Serovy, George K.
March 15, 1954
Primary view of A Flight Investigation of the Effects of Inclination of the Principal Axis of Inertia on the Dynamic Lateral Stability of the Republic XF-91 Airplane
Finch, Thomas W.
July 15, 1954
Primary view of Experimental Determination of Boundary-Layer Transition on a Body of Revolution at M = 3.5
Jedlicka, James R.; Wilkins, Max E. & Seiff, Alvin
March 15, 1954
Primary view of An Experimental Investigation of Four Triangular-Wing-Body Combinations in Sideslip at Mach Numbers 0.6, 0.9, 1.4, and 1.7
Christensen, Frederik B.
March 15, 1954
Primary view of Low-Speed Cascade Tests of Two 45 Degree Swept Compressor Blades With Constant Spanwise Loading
Beatty, Loren A.; Savage, Melvyn & Emery, James C.
March 15, 1954
Primary view of Rocket-Powered Model Investigation of Lift, Drag, and Stability of a Body-Tail Configuration at Mach Numbers From 0.8 to 2.3 and Angles of Attack Between Plus or Minus 6.5 Degrees
Gillespie, Warren, Jr. & Dietz, Albert E.
April 15, 1954
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