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- 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
- Laminar friction and heat transfer at Mach numbers from 1 to 10
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution
- On the angular distribution of slip lines in polycrystalline aluminum alloy
- Compilation and review of effects of design parameters on ditching characteristics
- Investigation at low speed of the effectiveness and hinge moments of a constant-chord elevator on a large-scale triangular wing with section modification
- An investigation at Mach numbers of 1.40 and 1.59 of the effects of aileron profile on the aerodynamic characteristics of a complete model of a supersonic aircraft configuration
- Investigation of dynamic characteristics of a turbine-propeller engine
- The effect of thickness ratio on section thrust distribution as determined from a study of wake surveys of the NACA 4-(0)(03)-045 and 4-(0)(08)-045 two-blade propellers up to forward Mach numbers of 0.925
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 5: analysis and comparison on basis of ram-jet aircraft range and operational characteristics
- A comparison of the turbulent boundary-layer growth on an unswept and a swept wing
- Theoretical analysis of some simple types of acceleration restrictors
- The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing
- The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback
- The effects of camber and twist on the aerodynamic loading and stalling characteristics of a large-scale 45 degree swept-back wing
- Contributions of wing, tail, and fuselage to the aerodynamic characteristics of a semispan model of a supersonic airplane configuration at transonic speeds from tests by the NACA wing-flow method