National Advisory Committee for Aeronautics (NACA) - 158 Matching Results

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Primary view of Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Levine, Joseph & Kleinknecht, Kenneth S.
September 18, 1951
Primary view of Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
Dryer, Murray & Luidens, Roger W.
March 18, 1958
Primary view of Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing
Wiley, Harleth G.
November 18, 1952
Primary view of Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees
Kuhn, Richard E. & Draper, John W.
August 18, 1953
Primary view of Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds
Osborne, Robert S. & Wornom, Dewey E.
March 18, 1954
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device
Olson, Robert N. & Mead, Merrill H.
January 18, 1951
Primary view of Altitude Performance and Operational Characteristics of YJ71-A-7 Turbojet Engine
Smith, Ivan D.; Leonard, Charles V., Jr. & Bloomer, Harry E.
June 18, 1953
Primary view of Analyses for Turbojet Thrust Augmentation With Fuel-Rich Afterburning of Hydrogen, Diborane, and Hydrazine
Morris, James F.
June 18, 1957
Primary view of Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine
Morris, James F.
June 18, 1957
Primary view of Analysis and Construction of Design Charts for Turbines with Downstream Stators
Cavicchi, Richard H. & Constantine, Anita B.
November 18, 1954
Primary view of Analysis of an automatic control to prevent rolling divergence
Phillips, William H.
April 18, 1956
Primary view of Analysis of Limitations Imposed on One-Spool Ducted-Fan-Engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8
Cavicchi, Richard H.
July 18, 1957
Primary view of Analysis of two-stage counterrotating turbine efficiencies in terms of work and speed requirements
Wintucky, William T. & Stewart, Warner L.
March 18, 1958
Primary view of Analytical investigation of flow and heat transfer in coolant passages of free-convection liquid-cooled turbines
Eckert, E. R. G. & Jackson, Thomas W.
July 18, 1950
Primary view of Analytical investigation of multistage-turbine efficiency characteristics in terms of work and speed requirements
Stewart, Warner L.
February 18, 1958
Primary view of Analytical procedures for rapid selection of coolant passage configurations for air-cooled turbine rotor blades and for evaluation of heat-transfer, strength, and pressure-loss characteristics
Ziemer, Robert R. & Slone, Henry O.
September 18, 1952
Primary view of Application of non-afterburning turbojets to supersonic flight
Cesaro, Richard S. & Walker, Curtis L.
November 18, 1955
Primary view of Boundary-Layer Measurements on Several Porous Materials With Suction Applied
McCullough, George B. & Gambucci, Bruno J.
June 18, 1952
Primary view of Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7
Chauvin, Leo T. & Speegle, Katherine C.
April 18, 1957
Primary view of Calculation of Flutter Characteristics for Finite-Span Swept or Unswept Wings at Subsonic and Supersonic Speeds by a Modified Strip Analysis
Yates, E. Carson, Jr.
March 18, 1958
Primary view of Characteristics of a Transonic Test Section With Various Slot Shapes in the Langley 8-Foot High-Speed Tunnel
Wright, Ray H. & Ritchie, Virgil S.
October 18, 1951
Primary view of Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap
Croom, Delwin R.
December 18, 1952
Primary view of Cold-air investigation of a turbine with nontwisted rotor blades suitable for air cooling
Heaton, Thomas R.; Slivka, William R. & Westra, Leonard F.
March 18, 1952
Primary view of Combustor performance of a 16-inch ram jet using gaseous hydrogen as fuel at Mach number 3.0
Wasserbauer, Joseph F. & Wilcox, Fred A.
January 18, 1957
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