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- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- A method for determining core dimensions of heat exchanger with one dominating film resistance and verification with experimental data
- An inlet design concept to reduce flow distortion at angle of attack
- Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine
- Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades
- Flight measurements of airplane structural temperatures at supersonic speeds
- Survey of hydrogen combustion properties
- Analytical study of the equilibrium thickness of boric oxide deposits on jet-engine surfaces
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1
- Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
- Flutter at very high speeds
- Effects on adjacent surfaces from the firing of rocket jets
- Span loadings due to wing twist at transonic and supersonic speeds
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies
- Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01
- Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
- Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
- Transonic wind-tunnel investigation of aerodynamic-loading characteristics of a 2-percent-thick trapezoidal wing in combination with basic and indented bodies
- Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45©� high-wing model oscillating in yaw
- Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane
- Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶
- Heat transfer to bodies at angles of attack
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance
- Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
- Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds
- Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique
- Preliminary Internal Performance Data for a Variable-Ejector Assembly on the XJ79-GE-1 Turbojet Engine, II, Afterburning Configurations
- Turbulence in the Wake of a Thin Airfoil at Low Speeds
- Blow-Out Velocities of Solutions of Hydrocarbons and Boron Hydride - Hydrocarbon Reaction Products in a 1 7/8-Inch-Diameter Combustor
- A Fuselage Addition to Delay Drag-Rise Mach Number of Subsonic Airplanes at Lifting Conditions
- Surge-Inception Study in a Two-Spool Turbojet Engine, Revised
- Experimental Investigation of Vibratory Stresses in a Concentric-Ring Direct-Air-Cycle Nuclear Fuel Element
- Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair TF-102A Airplane at Transonic Speeds, Coord. No. AF-120
- High altitude performance investigation of J65-B-3 turbojet engine with both JP-4 and gaseous hydrogen fuels
- Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9
- Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing
- Design and performance of flight-type liquid-hydrogen heat exchanger
- Experimental Investigation of Effects of Combustion-chamber Length and Inlet Total Temperature, Total Pressure, and Velocity on Afterburner Performance
- Altitude free-jet investigation of dynamics of a 28-inch-diameter ram-jet engine
- Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine
- Reaction of fluorine with carbon as a means of fluorine disposal
- Investigation of Heat Transfer from a Stationary and Rotating Conical Forebody
- Experimental Droplet Impingement on Four Bodies of Revolution
- Free-Flight Skin Temperature and Pressure Measurements on a Slightly Blunted 25 Deg Cone-Cylinder-Flare Configuration to a Mach Number of 9.89
- Statistical Study of Aircraft Icing Probabilities at the 700- and 500- Millibar Levels over Ocean Areas in the Northern Hemisphere