National Advisory Committee for Aeronautics (NACA) - 12 Matching Results

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Primary view of Analysis of V-g data obtained from several naval airplanes
Thornton, James O.
July 7, 1950
Primary view of The Calculation of the Path of a Jettisonable Nose Section
Goodwin, Roscoe H.
September 7, 1950
Primary view of Determination of Longitudinal Stability of the Bell X-1 Airplane From Transient Responses at Mach Numbers Up to 1.12 at Lift Coefficients of 0.3 and 0.6
Angle, Ellwyn E. & Holleman, Euclid C.
November 7, 1950
Primary view of The Effect of Changes in the Leading-Edge Radius on the Aerodynamic Characteristics of a Symmetrical, 9-Percent-Thick Airfoil at High-Subsonic Mach Numbers
Humphreys, Milton D. & Robinson, Raymond A.
August 7, 1950
Primary view of Effect of compressor-outlet bleedoff on turbojet-engine performance
Fleming, William A.; Wallner, Lewis E. & Wintler, John T.
August 7, 1950
Primary view of Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane
Heinle, Donovan R.
December 7, 1950
Primary view of An investigation of three transonic fuselage air inlets at Mach numbers from 0.4 to 0.94 and at a Mach number of 1.19
Pendley, Robert E.; Robinson, Harold L. & Williams, Claude V.
November 7, 1950
Primary view of Lateral-Control Investigation at a Reynolds Number of 5,300,000 of a Wing of Aspect Ratio 5.8 Sweptforward 32 Degrees at the Leading Edge
Graham, Robert R.
February 7, 1950
Primary view of Low-Speed Pressure-Distribution Measurements at Reynolds Number of 3.5 X 10(Exp 6) on a Wing With Leading-Edge Sweepback Decreasing From 45 Degrees at the Root to 20 Degrees at the Tip
Barnett, U. Reed, Jr. & Lange, Roy H.
July 7, 1950
Primary view of Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 2: Methods for Determining Cooling-Air-Flow Characteristics
Ellerbrock, Herman H., Jr.
June 7, 1950
Primary view of Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
Frank, Joseph L.
July 7, 1950
Primary view of Summary of the Aerodynamic Characteristics and Flying Qualities Obtained from Flights of Rocket-Propelled Models of an Airplane Configuration Incorporating a Sweptback Inversely Tapered Wing at Transonic and Low-Supersonic Speeds
Mitcham, Grady L. & Blanchard, Willard S., Jr.
September 7, 1950
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