National Advisory Committee for Aeronautics (NACA) - 41 Matching Results

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Primary view of Flight tests of thermal ice-prevention equipment in the XB-24F airplane
Neel, Carr B. & Jones, Alun R.
October 7, 1943
Primary view of Drag Measurements of Symmetrical Circular-Arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
Alexander, Sidney R.
March 7, 1947
Primary view of Theoretical analysis of the motions of an aircraft stabilized in roll by a displacement-response, flicker-type automatic pilot
Curfman, Howard J., Jr. & Gardner, William N.
July 7, 1948
Primary view of Preliminary full-scale investigation of a 1/3-scale model of a convertible-type airplane
Lange, Roy H.; Cocke, Bennie W., Jr. & Proterra, Anthony J.
June 7, 1949
Primary view of A comparison of the simulated-altitude performance of two turbojet combustor types
Bolz, Ray E.; Schroeter, Thomas T. & Zettle, Eugene V.
October 7, 1948
Primary view of Pressure-distribution measurements over an extensible leading-edge flap on two wings having leading-edge sweep of 42 degrees and 52 degrees
Salmi, Reino J.
March 7, 1949
Primary view of Wing-Tunnel Investigation at High Subsonic Speeds of the Lateral-Control Characteristics of an Aileron and a Stepped Spoiler on a Wing With Leading Edge Swept Back 51.3 Degrees
Schneiter, Leslie E. & Hagerman, John R.
June 7, 1949
Primary view of Preliminary investigation of combustion in flowing gas with various turbulence promoters
Haddock, Gordon W. & Childs, J. Howard
June 7, 1948
Primary view of Aerodynamic Characteristics of an 0.08-Scale Model of the Martin XB-51 Airplane at High Subsonic Speeds
Barnes, Robert H.
October 7, 1949
Primary view of Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9
Conner, D. William & May, Ellery B., Jr.
October 7, 1949
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail
McCormack, Gerald M.
October 7, 1949
Primary view of Effect of Number of Fins on the Drag of a Pointed Body of Revolution at Low Supersonic Velocities
Mastrocola, N.
April 7, 1947
Primary view of Test-stand investigation of a rectangular ram-jet engine
Black, Dugald O. & Messing, Wesley E.
May 7, 1947
Primary view of Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds
Turner, Thomas R.; Lockwood, Vernard E. & Vogler, Raymond D.
September 7, 1948
Primary view of Investigation of ceramic, graphite, and chrome-plated graphite nozzles on rocket engine
Kinney, George R. & Lidman, William G.
March 7, 1949
Primary view of Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5
Perkins, Edward W.
May 7, 1948
Primary view of Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine
Acker, Loren W. & Kleinknecht, Kenneth S.
April 7, 1949
Primary view of The Effect of Air Jets Simulating Chines or Multiple Steps on the Hydrodynamic Characteristics of a Streamline Fuselage
Weinflash, Bernard
January 7, 1949
Primary view of Ditching tests of a 1/15-scale model of the Fairchild C-82 airplane
Fisher, Lloyd J. & Hoffman, Edward L.
October 7, 1948
Primary view of Method of Determining Centrifugal-Flow-Compressor Performance With Water Injection
Hamrick, Joseph T. & Beede, William L.
September 7, 1949
Primary view of Comparison of the Aerodynamic Characteristics of the NACA 0010 and 0010-64 Airfoil Sections at High Subsonic Mach Numbers
Polentz, Perry P.
October 7, 1949
Primary view of A Preliminary Investigation of the Usefulness of Camber in Obtaining Favorable Airfoil-Section Drag Characteristics at Supercritical Speeds
Nitzberg, Gerald E.; Crandall, Stewart M. & Polentz, Perry P.
October 7, 1949
Primary view of Static longitudinal stability and control of a convertible-type airplane as affected by articulated- and rigid-propeller operation
Lange, Roy H. & McLemore, Huel C.
November 7, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Characteristics for Symmetrical Wing Sections at High Subsonic and Moderate Supersonic Mach Numbers
Mas, Newton A.
July 7, 1949
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