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- Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying
- Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively
- Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5
- Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants
- Experimental investigation of axial and normal force characteristics of skewed nozzles
- Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing
- Experimental investigation of an impulse-type supersonic compressor rotor having a turning of 73 degrees at the mean radius
- Jet effects on the base drag of a cylindrical afterbody with extended nozzles
- Dilution of liquid oxygen when nitrogen is used for pressurization
- Performance of an All-Internal Conical Compression Inlet with Annular Throat Bleed at Mach Number 5.0
- A numerical method for evaluating wave drag
- Physical characteristics and test conditions of an ethylene-heated high-temperature jet
- Observations of turbulent-burst geometry and growth in supersonic flow
- Some effects of flow spoilers and of aerodynamic balance on the oscillating hinge moments for a swept fin-rudder combination in a transonic wind tunnel
- Preliminary performance data obtained in a full-scale, free-jet investigation of a side-inlet supersonic diffuser
- Thin airfoil theory based on approximate solution of the transonic flow equation
- Wind-tunnel tests of a full-scale helicopter rotor with symmetrical and with cambered blade sections at advance ratios from 0.3 to 0.4
- Analytical and experimental investigation of a temperature-schedule acceleration control for a turbojet engine
- Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube
- Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties
- Use of the Coanda effect for obtaining jet deflection and lift with a single flat-plate deflection surface
- Use of the Coanda effect for jet deflection and vertical lift with multiple-flat-plate and curved-plate deflection surfaces
- Use of the Kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model
- Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20
- Analysis of transonic rotor-blade passage loss with hot-wire anemometers
- An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection
- An approximate analytical method for studying entry into planetary atmospheres
- Turbulent boundary layer on a yawed cone in a supersonic stream
- Wind-tunnel investigation of the high-subsonic static longitudinal stability characteristics of several wing-body configurations designed for high lift-drag ratios at a Mach number of 1.4
- Wind-tunnel investigation of the static longitudinal stability and trim characteristics of a sweptback-wing jet-transport model equipped with an external-flow jet augmented flap
- Flight investigation of the low-speed characteristics of a 45 degree swept-wing fighter-type airplane with blowing boundary-layer control applied to the trailing edge flaps
- Experimental investigation of a high subsonic Mach number turbine having a 40-blade rotor with zero suction-surface diffusion
- Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8
- Free-flight transonic model investigation of jet effects on a fighter-type configuration employing a tail boom and three horizontal-tail positions
- Investigation of boiling burnout and flow stability for water flowing in tubes
- The rate of fatigue-crack propagation in two aluminum alloys
- Effect of sliding velocity on friction properties and endurance life of bonded lead monoxide coatings at temperatures up to 1250 F
- Collection of zero-lift drag data on bodies of revolution from free-flight investigations
- Effects of fabrication-type roughness on turbulent skin friction at supersonic speeds
- Effects of fixing boundary-layer transition for an unswept-wing model and an evaluation of porous tunnel-wall interference for Mach numbers from 0.60 to 1.40
- Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M=5.0
- Effect of screens in reducing distortion and diffusion length for a 'dump' diffuser at a Mach number of 3.85
- Effect of jet temperature on jet-noise generation
- An analysis of surface pressures and aerodynamic load distribution over the swept wing of the Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73
- Application of a high-temperature static strain gage to the measurement of thermal stresses in a turbine stator vane
- Application of statistical theory to beam-rider guidance in the presence of noise 2: modified Wiener filter theory
- Measurements of total hemispherical emissivity of various oxidized metals at high temperature
- Measurements of ground-reaction forces and vertical center-of-gravity accelerations of a bomber airplane taxiing over obstacles
- Study of ground-reaction forces measured during landing impacts of a large airplane
- Wind-tunnel investigation of effects of spoiler location, spoiler size, and fuselage nose shape on directional characteristics of a model of a tandem-rotor helicopter fuselage