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- Comparison between flight-measured and calculated span load distribution at high Mach numbers
- The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions
- Investigation of Thrust Augmentation of a 1600-Pound Thrust Centrifugal-Flow-Type Turbojet Engine by Injection of Refrigerants at Compressor Inlets
- Measurements of the damping in roll of large-scale swept-forward and swept-back wings
- Fuel investigation in a tubular-type combustor of a turbojet engine
- Preliminary investigation of effects of alpha-particle bombardment on the creep rate of aluminum
- A suggested method of analyzing for transonic flutter of control surfaces based on available experimental evidence
- Fuel tests on an I-16 jet-propulsion engine at static sea-level conditions
- A fuel-distribution control for continuous-flow manifold injection on reciprocating engines
- The use of perforated inlets for efficient supersonic diffusion
- An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane
- Characteristics of a 15-percent-chord and a 35-percent-chord plain flap on the NACA 0006 airfoil section at high subsonic speeds
- Combustion-efficiency investigation of special fuels in single tubular-type combustor at simulated altitude conditions
- Computed performance of a composite engine based on experimental data for a single-cylinder conventional aircraft engine converted to compression-ignition operation
- Flight investigation of the heat requirements for ice prevention on aircraft windshields
- A summary report on the effects of Mach number on the span load distribution on wings of several models
- Aerodynamic measurements made during Navy investigation of human tolerance to wind blasts
- Theoretical investigation of thrust augmentation of turbojet engines by tail-pipe burning
- Performance of a 20-inch steady-flow ram jet at high altitudes and ram-pressure ratios
- High-speed wind-tunnel investigation of the effects of compressibility on a pitot-static tube
- An empirically derived method for calculating pressure distribution at supercritical Mach numbers and moderate angles of attack
- Knock-limited power outputs from a CFR engine using internal coolants III : four alkyl amines, three alkanolamines six amides, and eight heterocyclic compounds
- Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number 1.5
- An investigation of the effect of tip shape on the low-speed aerodynamic characteristics of large-scale swept wings
- Analytical comparison of a standard turbojet engine, a turbojet engine with a tail-pipe burner, and a ram-jet engine
- Investigation of carbon deposition in an I-16 jet-propulsion engine at static sea-level conditions
- Cooling of gas-turbines 7: effectiveness of air cooling of hollow turbine blades with inserts
- Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine II: performance with water injection at compressor inlet
- Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe
- Application of an ultraviolet spectrophotometric method to the estimation of alkylnaphthalenes in 10 experimental jet-propulsion fuels
- Experimental investigation of performance and operating characteristics of a tail-pipe burner for a turbojet engine
- An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane
- Investigation of wing characteristics at a Mach number of 1.53 1: triangular wings of aspect ratio 2
- The calculation of drag for airfoil sections and bodies of revolution at subcritical speeds
- Investigation of shock diffusers at Mach number 1.85 2: projecting double-shock cones
- Investigation of shock diffusers at Mach number 1.85 3: multiple-shock and curved-contour projecting cones
- An approximate method for calculating the effect of surface roughness on the drag of an airplane
- An Investigation of Convergent-Divergent Diffusers at Mach Number 1.85
- A comparison with flight data of vertical-tail loads in various maneuvers estimated from sideslip angles and rudder deflections
- Experimental investigation of thrust augmentation of a turbojet engine at zero ram by means of tail-pipe burning
- Test-stand investigation of a rectangular ram-jet engine
- A summary and analysis of data on dive-recovery flaps
- Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness
- Wing-flow tests of a triangular wing of aspect ratio two 1: effectiveness of several types of trailing-edge flaps on flat-plate models
- Investigation of Rim Cracking in Turbine Wheels with Welded Blades
- Stick-Fixed Stability and Control Characteristics of the Consolidated Vultee Model 240 Airplane as Estimated from Tests of a 0.092-Scale Powered Model
- Flight Comparison of Performance and Cooling Characteristics of Exhaust-Ejector Installation with Exhaust-Collector-Ring Installation
- Cooling of Gas Turbines, 2, Effectiveness of Rim Cooling of Blades
- High-altitude flight cooling investigation of a radial air-cooled engine
- Interference method for obtaining the potential flow past an arbitrary cascade of airfoils