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- Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient
- Flight tests of experimental beveled-trailing-edge Frise ailerons on a fighter airplane
- Flutter and oscillating air-force calculations for an airfoil in two-dimensional supersonic flow
- Flow over a slender body of revolution at supersonic velocities
- Theoretical lift and drag of thin triangular wings at supersonic speeds
- Tank tests to determine the effect on planing-tail hulls of varying length, width, and plan-form taper of afterbody
- Summary of lateral-control research
- Two dimensional wind-tunnel investigation of low drag vertical-tail,horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces
- Wind-tunnel investigation of end-plate effects of horizontal tails on a vertical tail compared with available theory
- The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates
- Analysis of Available Data on the Effects of Tabs on Control-Surface Hinge Moments
- Analysis of Deep Rectangular Shear Web Above Buckling Load
- Effect of Distance on Airplane Noise
- Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane
- An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane
- Influence of wall boundary layer upon the performance of an axial-flow fan rotor
- The effect of high solidity on propeller characteristics at high forward speeds from wind-tunnel tests of the NACA 4-(3)(06.3)-06 and NACA 4-(3)(06.4)-09 two-blade propellers
- Performance of compressor blade cascades at high Mach numbers
- The NACA mixture analyzer and its application to mixture-distribution measurement in flight
- Some Recent Contributions to the Study of Transition and Turbulent Boundary Layers
- An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel. Part IV - Aileron Characteristics TED No. NACA DE308, Part 4, Aileron Characteristics, TED No. NACA DE308
- High-Speed Load Distribution of the Wing of a 3/16-Scale Model of the Douglas XSB2D-1 Airplane with Flaps Deflected
- Effect of Exhaust Pressure on the Cooling Characteristics of a Liquid-Cooled Engine
- Wind-Tunnel Investigation of the Low-Speed Characteristics of a 1/8-Scale Model of the Republic XP-91 Airplane with a Vee and a Conventional Tail
- The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil
- Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XP-85 Airplane While Attached to the Trapeze
- Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Static Longitudinal Stability of Models with Wing Flap Deflections of 0 Deg and 15 Deg, TED No. NACA 2387
- Recent Results on High-Pressure Axial Blowers
- Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed
- Pressure Distribution Measurements at High Speed and Oblique Incidence of Flow
- Lift and Drag of Wings with Small Span
- Possibilities of Reducing the Length of Axial Superchargers for Aircraft Motors
- Cooling of Gas Turbines, IV - Calculated Temperature Distribution in the Trailing Part of a Turbine Blade Using Direct Liquid Cooling
- Effects of Compressibility on the Flow Past Thick Airfoil Sections
- An Anaylsis of Control Requirements and Control Parameters for Direct-Coupled Turbojet Engines
- Preliminary Evaluation of the Low-Speed Stability and Control Characteristics of the McDonnell XP-85 Airplane from Tests of an Unballasted 1/5-Scale Model in the Langley Free-Flight Tunnel
- Preliminary Evaluation of the Spin and Recovery Characteristics of the Douglas XF3D-1 Airplane
- High-Speed Load Distribution on the Wing of a 3/16-Scale Model of a Scout-Bomber Airplane with Flaps Deflected
- A Comparison of Three Theoretical Methods of Calculating Span Load Distribution on Swept Wings
- 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