Search Results

Primary view of [Stan Kenton observing banner]
unknown creator
1952-05-20/1952-05-25
Primary view of [Kenton observing jewelry box]
Scibilia, James
1952-05-20/1952-05-25
Primary view of Tracking Performance of a Swept-Wing Fighter With a Director-Type Radar Fire-Control System and Scope Presentation
Turner, Horward L.; Rathert, George A., Jr. & Heinle, Donovan R.
January 20, 1958
Primary view of Performance of Variable Two-Dimensional Inlet Designed for Engine-Inlet Matching 1 - Performance at Design Mach Number of 3.07
Beheim, M. A. & Gertsma, L. W.
November 20, 1956
Primary view of Performance at Mach Numbers 3.07, 1.89, and 0 of Inlets Designed for Inlet-Engine Matching Up to Mach 3
Gertsma, L. W. & Beheim, M. A.
May 20, 1958
Primary view of Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
Phelps, E. Ray
April 20, 1956
Primary view of Altitude Performance of a Turbojet Engine Using Pentaborane Fuel
Sivo, Joseph N.
May 20, 1957
Primary view of Performance of Pentaborane, Pentaborane - JP-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-scale Turbojet Engine
Breitwieser, Roland & Useller, James W.
November 20, 1956
Primary view of Experimental Investigation of a High Subsonic Mach Number Turbine Having High Rotor Blade Suction-Surface Diffusion
Nusbaum, William J. & Hauser, Cavour H.
November 20, 1956
Primary view of Operation of an Experimental Air-Cooled Turbojet Engine at Turbine-Inlet Temperatures From 2200 R to 2935 R
Cochran, Reeves P.; Dengler, Robert P. & Esgar, Jack B.
August 20, 1956
Primary view of A Heated-Wire Liquid-Water-Content Instrument and Results of Initial Flight Tests in Icing Conditions
Neel, Carr B.
January 20, 1955
Primary view of Experimental Investigation of Radome Icing and Icing Protection
Lewis, James P. & Blade, Robert J.
January 20, 1953
Primary view of Canard Hinge Moments and Longitudinal Stability of a 1/7-Scale Model of the Convair B-58 External Store in a Free-Flight Investigation at Mach Numbers From 0.94 to 2.58
Hollinger, James A.
June 20, 1958
Primary view of Transonic Wind-Tunnel Tests of the Launch, Jettison, and Longitudinal Characteristics of an Airplane and Missile Model Combination
Cleary, Joseph W.; Frank, Joseph L. & Dewey, C. Forbes, Jr.
November 20, 1957
Primary view of Investigation of Ejection Releases of an MB-1 Rocket From a 0.04956-Scaled Model of the Convair F-106A Airplane at Mach Number 1.59
Lee, John B.
May 20, 1957
Primary view of Investigation of Ejection Releases of an MB-1 Rocket From a 0.04956-Scaled Model of the Convair F-106A Airplane at Mach Number 1.59
Lee, John B.
May 20, 1957
Primary view of Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane
Fisher, Lloyd J. & Morris, Garland J.
April 20, 1950
Primary view of An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc section and 40 degree sweepback: a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.40
Smith, Norman F.; Kainer, Julian H. & Webster, Robert A.
April 20, 1951
Primary view of Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
Stivers, Louis S., Jr.; Walker, Harold J. & Beard, Luther, Jr.
April 20, 1951
Primary view of Review of Current and Anticipated Lubricant Problems in Turbojet Engines
unknown creator
April 20, 1951
Primary view of Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids
Jackson, Joseph L.
December 20, 1950
Primary view of Tabulated pressure coefficients and aerodynamic characteristics measured on the wing of the Bell X-1 airplane in an unaccelerated low-speed stall, in push-overs at Mach numbers of 0.83 and 0.99, and in a pull-up at a Mach number of 1.16
Knapp, Ronald J.
September 20, 1951
Primary view of Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the D-558-I Research Airplane Through a Mach Number Range of 0.80 to 0.89 and Throughout the Normal-Force-Coefficient Range at Mach Numbers of 0.61, 0.70, 0.855, and 0.88
Keener, Earl R. & Bandish, Rozalia M.
August 20, 1951
Primary view of The Effect on Zero-Lift Drag of an Indented Fuselage or a Thickened Wing-Root Modification to a 45 Degree Sweptback Wing-Body Configuration as Determined by Flight Tests at Transonic Speeds
Pepper, William B.
September 20, 1951
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