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- Tank investigation of the Grumman JRF-5 airplane with a single hydro-ski and an extended afterbody
- Altitude investigation of 16 flame-holder and fuel-system configurations in tail-pipe burner
- The transonic characteristics of 17 rectangular, symmetrical wing models of varying aspect ratio and thickness
- A theoretical investigation of the influence of autopilot natural frequency upon the dynamic performance characteristics of a supersonic canard missile configuration with a pitch-attitude control system
- Wind-tunnel investigation of six shielded total-pressure tubes at high angles of attack: Subsonic speeds
- Altitude-wind-tunnel investigation of performance characteristics of a J47D prototype (RX1-1) turbojet engine with variable-area exhaust nozzle
- Altitude-test-chamber investigation of performance of a 28-inch ram-jet engine 3: combustion and operational performance of three flame holders with a center pilot burner
- The torsional deflections of several propellers under operating conditions
- Minimum wave drag of bodies of revolution with a cylindrical center section
- Performance characteristics of aircraft cooling ejectors having short cylindrical shrouds
- Stability and control characteristics at low speed of a 1/5-scale model of the Edo 142 hydro-ski research airplane
- Preliminary investigation of molybdenum disulfide-air-mist lubrication for roller bearings operating to DN values of 1 x 10(exp 6) and ball bearings operating to temperatures of 1000 degrees F
- Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
- Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing, both having 45 degrees of sweepback
- 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
- Experimental evaluation by thermodynamic methods of work input to a centrifugal compressor operating with water injection
- Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls with Application to Turbine Blade Cooling
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 III : conical-spike all-external-compression inlet with supersonic cowl lip
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 1: conical spike all-external compression inlet with subsonic cowl lip
- Fatigue strengths of aircraft materials: axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factors of 2.0 and 4.0
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device
- Preliminary investigation of the delay of turbulent flow separation by means of wedge-shaped bodies
- Preliminary investigation of the supersonic flow field downstream of wire-mesh nozzles in a constant-area duct / Lawrence I. Gould
- Some effects of solidity on turning through constant-thickness circular-arc guide vanes in axial annular flow
- Studies of high-temperature protection of a titanium-carbide ceramal by chromium-type ceramic-metal coatings
- Review of some recent data on buffet boundaries
- Transonic flow past a wedge profile with detached bow wave : details of analysis
- Wing-flow investigation of the characteristics of seven unswept, untapered airfoils of aspect ratio 8.0
- Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with self-supporting free-floating fuel tanks attached to the wing tips
- Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a tip-to-tip bomber-fighter coupled airplane configuration
- Investigation of annular liquid flow with concurrent air flow in horizontal tubes
- An investigation of the spray characteristics of a jet-powered dynamic model of the drag flying boat with a vee tail : TED No. NACA DE 328
- Free-flight performance of 16-inch diameter supersonic ram-jet units 4: performance of ram-jet units designed for combustion chamber inlet Mach number of 0.21 at free-stream Mach number of 1.6 over a range flight conditions
- A comparison of the experimental and theoretical loading over triangular wings in sideslip at supersonic speeds
- A comparison of the calculated maximum-maneuver response characteristics of three air-to-air, beam-rider, guided missiles having different lift ratios
- A comparison of the experimental and theoretical loading over triangular wings at supersonic speeds
- Effect of blade-surface finish on performance of a single-stage axial-flow compressor
- Design and performance of an experimental axial-discharge mixed-flow compressor II : over-all performance of impeller and supersonic-diffuser combination
- Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52
- Effects of spanwise thickness variation on the transonic aerodynamic characteristics of wings having 35 degrees of sweepback, aspect ratio 4, and taper ratio 0.60
- Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method
- Application of Theodorsen's propeller theory to the calculation of the performance of dual-rotating propellers
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution, cambered and twisted for a trapezoidal span load distribution
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: twisted and cambered triangular wing of aspect ratio 2 with NACA 0003-63 thickness distribution
- A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers
- Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder
- An investigation of convergent-divergent diffusers at Mach number 1.85
- Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration
- A velocity-correction formula for the calculation of transonic Mach number distributions over diamond-shaped airfoils
- Velocity and temperature fields in circular jet expanding from choked nozzle into quiescent air