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Primary view of NACA Conference on High-Speed Aerodynamics: A Compilation of Papers Presented
unknown creator
1958-03-18/1958-03-20
Primary view of Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85
Dickey, Robert R. & Spahr, J. Richard
March 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 Experimental Investigation of a Body Flare for Obtaining Pitch Stability and a Body Flap for Obtaining Pitch Control in Hypersonic Flight
Eggers, A. J., Jr. & Syvertson, Clarence A.
January 18, 1955
Primary view of Reaction of Fluorine With Carbon as a Means of Fluorine Disposal
Schmidt, Harold W.
July 18, 1957
Primary view of Development of a Supersonic Area Rule and an Application to the Design of a Wing-Body Combination Having High Lift-to-Drag Ratios
Whitcomb, Richard T. & Fischetti, Thomas L.
August 18, 1953
Primary view of Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a Model of a 40.4 Degree Swept-Wing Airplane at Mach Numbers of 1.56 and 2.06
Carmel, Melvin M. & Turner, Kenneth L.
January 18, 1957
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 Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Levine, Joseph & Kleinknecht, Kenneth S.
September 18, 1951
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 Spark Ignition of Flowing Gases. 2: Effect of Electrode Parameters on Energy Required to Ignite a Propane-Air Mixture
Swett, Clyde C., Jr.
December 18, 1951
Primary view of Investigation of Two Bluff Shapes in Axial Free Flight Over a Mach Number Range From 0.35 to 2.15
Coltrane, Lucille C.
March 18, 1958
Primary view of Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 2 - Design and Experimental Performance of Turbine With Low-Velocity-Turning Stator and Standard Rotor
Rohlik, Harold E.; Wintucky, William T. & Scibbe, Herbert W.
July 18, 1957
Primary view of An Investigation of the Effects of Nose and Lip Shapes for an Underslung Scoop Inlet at Mach Numbers from 0 to 1.9
Pfyl, Frank A.
November 18, 1955
Primary view of Some Design and Operational Considerations of a Liquid-Hydrogen Fuel and Heat-Sink System for Turbojet-Engine Tests
Corrington, Lester C.; Thornbury, Kenneth L. & Hennings, Glen
December 18, 1956
Primary view of Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conductive to Low Transonic Drag Rise
Hopko, Russell N.; Piland, Robert O. & Hall, James R.
November 18, 1953
Primary view of Experimental Behavior of Pentaborane-Air Combustion Products During Expansion in a Convergent Divergent Nozzle
Branstetter, J. Robert & Setze, Paul C.
February 18, 1958
Primary view of Lateral-control investigation of flap-type and spoiler-type controls on a wing with quarter-chord-line sweepback of 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method
Hammond, Alexander D.
July 18, 1950
Primary view of The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
Rathert, George A., Jr.; Rolls, L. Stewart & Hanson, Carl M.
August 18, 1950
Primary view of Pressure Distributions on the Blade Sections of the NACA 10-(5)(066)-03 Propeller Under Operating Conditions
Evans, Albert J. & Luchuk, Wallace
April 18, 1950
Primary view of Pressure Distributions on the Blade Sections of the NACA 10-(0)(066)-03 Propeller Under Operating Conditions
Steinberg, Seymour & Milling, Robert W.
May 18, 1950
Primary view of Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees
Fischel, Jack & Hammond, Alexander D.
January 18, 1950
Primary view of Ditching Tests With a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
Fisher, Lloyd J. & Tarshis, Robert P.
May 18, 1950
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
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