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Primary view of A Transonic Wing Investigation in the Langley 8-Foot High-Speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-Fuselage Configuration Having a Wing of 35 Degrees Sweepback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
Henry, Beverly Z., Jr.
November 15, 1950
Primary view of Experimental investigation of a flat plate paddle jet vane operating on a rocket jet
Bond, Aleck C.
November 15, 1950
Primary view of Method of Matching Performance of Compressor Systems with that of Aircraft Power Sections
Bullock, Robert O.; Keetch, Robert C. & Moses, Jason J.
November 15, 1945
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 Full-Scale-Wind-Tunnel Tests of a 35 Degree Sweptback Wing Airplane With High-Velocity Blowing Over the Training-Edge Flaps
Kelly, Mark W. & Tolhurst, William H., Jr.
November 15, 1955
Primary view of Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers From 0.70 to 1.96, Including an Evaluation of Techniques Used
Guy, Lawrence D. & Hadaway, William M.
November 15, 1955
Primary view of Effect of Fuel Composition, Engine Operating Variables, and Spark-Plug Type and Condition on Preignition-Limited Performance of an R-2800 Cylinder
Pfender, John F.
November 15, 1946
Primary view of Hydrodynamic Qualities of a 1/10-Size Powered Dynamic Model of the XP5Y-1 Flying Boat in Smooth Water: Langley Tank Model 246, TED No. NACA DE 320
Woodward, David R.; Weinstein, Irving & Whitaker, Walter E., Jr.
November 15, 1949
Primary view of Altitude-wind-tunnel investigation of J47 turbojet-engine performance
Conrad, E. William & Sobolewski, Adam E.
November 15, 1949
Primary view of Lateral-control investigation at transonic speeds of differentially deflected horizontal-tail surfaces for a configuration having a 6-percent-thick 45 degree sweptback wing
Critzos, Chris C.
November 15, 1955
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 Investigation of the Effect of Sweep on the Flutter of Cantilever Wings
Barmby, J. G.; Cunningham, H. J. & Garrick, I. E.
November 15, 1948
Primary view of Stability and control characteristics of a free-flying model with an unswept wing of aspect ratio 3 (XS-3)
Bennett, Charles V. & Hassell, James L., Jr.
November 15, 1948
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 Wind-tunnel investigation at subsonic and supersonic speeds of a fighter model employing a low-aspect-ratio unswept wing and a horizontal tail mounted well above the wing plane - longitudinal stability and control
Smith, Willard G.
November 15, 1954
Primary view of Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section
Vitale, A. James & McFall, John C., Jr.
November 15, 1954
Primary view of Full-scale performance study of a prototype crash-fire protection system for reciprocating-engine-powered airplanes
Black, Dugald O. & Moser, Jacob C.
November 15, 1955
Primary view of Effect of fuel-air ratio, inlet temperature, and exhaust pressure on detonation
Taylor, E. S.; Leary, W. A. & Diver, J. R.
November 15, 1939
Primary view of Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics
Evvard, John C. & Wyatt, DeMarquis D.
November 15, 1948
Primary view of Army Gas-Cooled Reactor Systems Program Quarterly Progress Report: July 1 - September 30, 1963
Aerojet-General Corporation
November 15, 1963
Primary view of Plutonium Recycle Test Reactor Final Safeguard Analysis: Supplement 2, Consequences of a Primary Coolant Leak
Wittenbrock, N. G. & Muraoka, J.
November 15, 1960
Primary view of A Mechanism for Automatic and Manual Control of the Air Velocity at the Window Opening of Fume Hoods
Weber, John, Jr.
November 15, 1948
Primary view of Reactor Physics Primer
Lockwood, E. H.
November 15, 1957
Primary view of Plating Thickness Tester
Fitch, C. E., Jr.
November 15, 1957
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