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- Free-Flight Tests of 0.11-Scale North American F-100 Airplane Wings to Investigate the Possibility of Flutter in Transonic Speed Range at Varying Angles of Attack
- Free-Flight Tests of 1/9-Scale Convair YF-102 Airplane Wings at Transonic and Supersonic Speeds to Investigate the Possibility of Flutter
- Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45©� sweptback wing at transonic speeds
- The twisting effect at transonic speeds of spoiler ailerons on a 45©� sweptback, aspect-ratio-4, tapered wing
- Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives
- Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4
- Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45©� sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶
- Theoretical investigation of some discontinuous yaw dampers
- Flight investigation of an aileron and a spoiler on a wing of the X-3 airplane plan form at Mach numbers from 0.5 to 1.6
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail
- Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine
- A Method for Prevention of Screaming in Rocket Engines
- Variation of Local Liquid-Water Concentration About and Ellipsoid of Fineness Ratio 5 Moving in a Droplet Field
- Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
- Analysis of rocket, ramjet, turbojet engines for supersonic propulsion of long-range missiles. 2: Rocket missile performance
- Analysis of rocket, ramjet, and turbojet engines for supersonic propulsion of long-range missiles. 3: Ramjet engine performance
- Combined Compressor Coolant Injection and Afterburning for Turbojet Thrust Augmentation
- Pumping Characteristics for Several Simulated Variablegeometry Ejectors With Hot and Cold Primary Flow
- Experimental Sea-Level Static Investigation of a Short Afterburner
- A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers
- Effect of Ice Formations on Section Drag of Swept NACA 63A-009 Airfoil with Partial-Span Leading-Edge Slat for Various Modes of Thermal Ice Protection
- A flight investigation of the practical problems associated with porous-leading-edge suction
- Investigation of Noise Field and Velocity Profiles of an Afterburning Engine
- Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds
- Investigation of an on-off inlet shock-position control on a 16-inch ram-jet engine
- The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane
- An exploratory investigation of skin friction and transition on three bodies of revolution at a Mach number of 1.61
- Investigation of Mach number changes obtained by discharging high-pressure pulse through wind tunnel operating supersonically
- An investigation of lamellar structures and minor phases in eleven cobalt-base alloys before and after heat treatment
- An investigation of a wing-propeller configuration employing large-chord plain flaps and large-diameter propellers for low-speed flight and vertical take-off
- An investigation of a lifting 10-percent-thick symmetrical double-wedge airfoil at mach number up to 1
- The influence of wheel spin-up on landing-gear impact
- Infrared spectra of 47 dicyclic hydrocarbons
- Investigation of static strength and creep behavior of an aluminum-alloy multiweb box beam at elevated temperatures
- Investigation of nickel-aluminum alloys containing from 14 to 34 percent aluminum
- A method for evaluating the effects of drag and inlet pressure recovery on propulsion-system performance
- A method for measuring the product of inertia and the inclination of the principal longitudinal axis of inertia of an airplane
- A method for estimating variations in the roots of the lateral-stability quartic due to changes in mass and aerodynamic parameters of an airplane
- Comparison between theory and experiment for interference pressure field between wing and body at supersonic speeds
- Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing
- A new method of analyzing extreme-value data
- A new hodograph for free-streamline theory
- Preliminary results from flow-field measurements around single and tandem rotors in the langley full-scale tunnel
- Present status of information relative to the prediction of shock-induced boundary-layer separation
- Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips : supersonic leading and trailing edges
- Liquefaction of air in the Langley 11-inch hypersonic tunnel
- Lift and moment coefficients expanded to the seventh power of frequency for oscillating rectangular wings in supersonic flow and applied to a specific flutter problem
- A further investigation of the effect of surface finish on fatigue properties at elevated temperatures
- Further studies of the mechanism by which hydrogen enters metals during chemical and electrochemical processing