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- Force Tests of the Boeing XB-47 Full-Scale Empennage in the Ames 40- by 80-Foot Wind Tunnel
- Performance of Compressor of XJ-41-V Turbojet Engine, 3, Compressor Static-Pressure Rise at Equivalent Compressor Speeds of 5000, 7000, 8000, and 9000 rpm
- Altitude Cooling Investigation of the R-2800-21 Engine in the P-47G Airplane. IV - Engine Cooling-Air Pressure Distribution
- Preliminary Investigation of Over-all Performance of Experimental Turbojet Engine for Guided Missiles
- Investigation of suction-slot shapes for controlling a turbulent boundary layer
- A method for numerically calculating the area and distribution of water impingement on the leading edge of an airfoil in a cloud
- Effects of sweepback on boundary layer and separation
- A method for calculating the heat required for windshield thermal ice prevention based on extensive flight tests in natural icing conditions
- Investigation of effects of surface temperature and single roughness elements on boundary-layer transition
- Flight tests of a double-hinged horizontal tail surface with reference to longitudinal-stability and control characteristics
- Flight measurements of the lateral control characteristics of narrow-chord ailerons on the trailing edge of a full-span slotted flap
- Interaction between the spars of semimonocoque wings with cutouts
- Instantaneous ultraviolet knock spectra correlated with high-speed photographs
- An investigation of valve-overlap scavenging over a wide range of inlet and exhaust pressures
- Method of designing vaneless diffusers and experimental investigation of certain undetermined parameters
- Notes and tables for use in the analysis of supersonic flow
- Effect of finite span on the airload distributions for oscillating wings. II - Methods of calculation and examples of application
- Effect of Finite Span on the Airload Distributions for Oscillating Wings I : Aerodynamic Theory of Oscillating Wings of Finite Span
- Effect of compressibility at high subsonic velocities on the moment acting on an elliptic cylinder
- Critical combinations of shear and direct stress for simply supported rectangular flat plates
- The effects of yawing thin pointed wings at supersonic speeds
- Changes found on run-in and scuffed surfaces of steel chrome plate, and cast iron
- Comparison of crystal structures of 10 wrought heat resisting alloys at elevated temperatures with their crystal structures at room temperatures
- Comparative performance of two vaneless diffusers designed with different rates of passage curvature for mixed-flow impellers
- Analysis of performance of jet engine from characteristics of components I : aerodynamic and matching characteristics of turbine component determined with cold air
- Boundary-layer momentum equations for three-dimensional flow
- The effect of preheating and postheating on the quality of spot welds in aluminum alloys
- Effect of product of inertia on lateral stability
- Propeller-efficiency charts for light airplanes
- A simplified method for elastic stability analysis for thin cylindrical shells II : modified equilibrium equation
- A simplified method of elastic-stability analysis for thin cylindrical shells I : Donnell's equation
- Experimental investigation of velocity distributions of downstream of single duct bends
- Subsonic flow over thin oblique airfoils at zero lift
- Formulas for additional mass corrections to the moments of inertia of airplanes
- Performance of a double-row radial aircraft engine with three methods of safety-fuel injection
- High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing
- Wind-tunnel investigation of the stability and control characteristics of a complete model equipped with a vee tail
- Wind-tunnel investigation of the boundary layer and wake and their relation to airfoil characteristics.NACA 65(sub 1)-012 airfoil with a true contour flap and a beveled-trailing-edge flap
- Critical stress of thin-walled cylinders in axial compression
- A comparison of three theoretical methods of calculating span load distribution on swept wings
- An application of lifting-surface theory to the prediction of angle-of-attack hinge-moment parameters for aspect ratio 4.5 wings
- Calculation of compressible flows past aerodynamic shapes by use of the streamline curvature
- Theoretical additional span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio
- Effects of temperature distribution and elastic properties of materials on gas-turbine-disk stresses
- The flow and force characteristics of supersonic airfoils at high subsonic speeds
- Wind-tunnel investigation of drooped ailerons on a 16-percent-thick low-drag airfoil
- High-altitude flight cooling investigation of a radial air-cooled engine
- Interference method for obtaining the potential flow past an arbitrary cascade of airfoils
- Interference of wing and fuselage from tests of 30 combinations with triangular and elliptical fuselages in the NACA variable-density tunnel
- Instability of outstanding flanges simply supported at one edge and reinforced by bulbs at other edge