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- 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
- The interdependence of various types of autoignition and knock
- Cooling Characteristics of the V-1650-7 Engine 2 - Effect of Coolant Conditions on Cylinder Temperatures and Heat Rejection at Several Engine Powers
- Cooling Characteristics of the V-1650-7 Engine, 1, Coolant-Flow Distribution, Cylinder Temperatures, and Heat Rejections at Typical Operating Conditions
- Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine. 5 - Performance of Modified Engine
- Buffeting of External Fuel Tanks at High Speeds on a Grumman F7F-3 Airplane
- Partial Measurements in Flight of the Flying Qualities of a Grumman XF7F-1 Airplane with a Modified Vertical Tail
- Buffeting of External Fuel Tanks at High Speeds on a Gruman F7F-3 Airplane
- Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8, and 19XB-1 Jet Propulsion Engines, 4 - Performance and Windmilling Drag Characteristics
- Acceleration Characteristics of R-3350 Engine Equipped with NACA Injection Impeller
- Determination of ram-jet combustion-chamber temperatures by means of total-pressure surveys
- Determination of elastic stresses in gas-turbine disks
- Effect of combustor-inlet conditions on performance of an annular turbojet combustor
- Effect of fuel on performance of a single combustor of an I-16 turbojet engine at simulated altitude conditions
- Design and performance of family of diffusing scrolls with mixed-flow impeller and vaneless diffuser
- Analysis of performance of jet engine from characteristics of components I : aerodynamic and matching characteristics of turbine component determined with cold air
- Analysis of effect of basic design variables on subsonic axial-flow-compressor performance
- Effects of sweepback on boundary layer and separation
- Altitude-Wind-Tunnel Investigation of R-4360-18 Power-Plant Installation for XR60 Airplane, 3, Performance of Induction and Exhaust Systems
- Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine 1 - Pressure and Temperature Distributions
- A simplified method of elastic-stability analysis for thin cylindrical shells
- Knock-Limited Performance of Triptane and 28-R Fuel Blends as Affected by Changes in Compression Ratio and in Engine Operating Variables
- Cooling of Gas Turbines, 3, Analysis of Rotor and Blade Temperatures in Liquid-Cooled Gas Turbines
- A Preliminary Study of Ram-Actuated Cooling Systems for Supersonic Aircraft
- Measurements in Flight of the Flying Qualities of a Chance Vought F4U-4 Airplane: TED No. NACA 2388
- Minimum Specific Fuel Consumption of a Liquid-Cooled Multicylinder Aircraft Engine as Affected by Compression Ratio and Engine Operating Conditions
- Performance of Compressor XJ-41-V Turbojet Engine 1 - Preliminary Investigation at Equivalent Compressor Speed of 8000 RPM
- Performance Investigation of TG-180 Combustor: 1 - Instrumentation, Altitude Operational Limits and Combustion Efficiency
- Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel. V - Operational Characteristics, 5, Operational Characteristics
- Isolated and cascade airfoils with prescribed velocity distribution
- Hydrodynamic impact of a system with a single elastic mode I : theory and generalized solution with an application to an elastic airframe
- Critical stress of thin-walled cylinders in axial compression
- Wing plan forms for high-speed flight
- Ditching Tests with a 1/12-Scale Model of the Army A-26 Airplane in Langley Tank No. 2 and on an Outdoor Catapult
- Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane
- Determination of Stress-Rupture Parameters for Four Heat-Resisting Alloys
- Effects of temperature distribution and elastic properties of materials on gas-turbine-disk stresses
- Preliminary Results of Altitude-Wind-Tunnel Investigation of X34C-4B Turbojet Engine. 3 - Compressor Performance, 3, Compressor Performance
- Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine. 4 - Performance of Modified Compressor, Part 4, Performance of Modified Compressor
- Investigation of pressure losses in several turbosupercharger nozzle hoses