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- Altitude-wind-tunnel investigation of J47 turbojet-engine performance
- Two-dimensional unsteady lift problems in supersonic flight
- Stability derivatives at supersonic speeds of thin rectangular wings with diagonals ahead of tip Mach lines
- Attainable circulation about airfoils in cascade
- The development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers
- Icing-protection requirements for reciprocating-engine induction system
- Effects of wing flexibility and variable air lift upon wing bending moment during landing impacts of a small seaplane
- Altitude-wind-tunnel investigation of various can-type burners in Bumblebee 18-inch ram jet
- Spark ignition of flowing gases I : energies to ignite propane-air mixtures in pressure range of 2 to 4 inches mercury absolute
- Appreciation and Prediction of Flying Qualities
- The design of low-turbulence wind tunnels
- Hovering and Low-Speed Performance and Control Characteristics of the Kaman Helicopter Rotor System as Determined on the Langley Helicopter Tower. TED No. NACA DE 205
- Laminar mixing of a compressible fluid
- Direct method of design and stress analysis of rotating disks with temperature gradient
- A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds
- Lecture Series "Boundary Layer Theory". Part I - Laminar Flows, Part 1, Laminar Flows
- Boundary Layer Theory, Part 2, Turbulent Flows
- An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape
- Performance of J33 turbojet engine with shaft-power extraction 3: turbine performance
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter)
- The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane
- Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness
- Performance of 24-inch supersonic axial-flow compressor in air 2: performance of compressor rotor at equivalent tip speeds from 800 to 1765 feet per second
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : characteristics at a Mach number of 1.53 including effect of small variations of sweep
- Study of the canard configuration with particular reference to transonic flight characteristics and low-speed characteristics at high lift
- Effect of screens in wide-angle diffusers
- The application of the statistical theory of extreme values to gust-load problems
- The effect of the propeller slipstream on the characteristics of submerged inlets
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Investigation of a large-scale model at low speed
- Experimental and Theoretical Studies of Area Suction for the Control of the Laminar Boundary Layer on a Porous Bronze NACA 64A010 Airfoil
- Moments of Cambered Round Bodies
- Investigations Relating to the Extension of Laminar Flow by Means of Boundary-Layer Suction Through Slots
- Observations of Icing Conditions Encountered in Flight During 1948
- Remarks Concerning the Behavior of the Laminar Boundary Layer in Compressible Flows
- Shear Buckling of Infinitely Long Simply Supported Metalite Type Sandwich Plates
- Provisional Symbols and Definitions for Aircraft Turbines
- Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design
- The Buckling of Parallel Simply Supported Tension and Compression Members Connected by Elastic Deflectional Springs
- The Response of Pressure Measuring Systems to Oscillating Pressures
- Notes on the Foundations of the Theory of Small Displacements of Orthotropic Shells
- Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds
- Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 40 Degrees
- Critical Combinations of Shear and Direct Axial Stress for Curved Rectangular Panels
- Wind-Tunnel Investigation of an NACA 65-210 Semispan Wing Equipped With Circular Plug Ailerons and a Full-Span Slotted Flap
- Theory of the Inlet and Exhaust Processes of Internal-Combustion Engines
- Summary of Information Relating to Gust Loads on Airplanes
- A Rapid Graphical Method for Computing the Pressure Distribution at Supersonic Speeds on a Slender Arbitrary Body of Revolution
- On Compressibility Corrections for Subsonic Flow Over Bodies of Revolution
- Observations on the Maximum Average Stress of Flat Plates Buckled in Edge Compression