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- On the Theory of Combustion of Initially Unmixed Gases
- Relations Between the Modulus of Elasticity of Binary Alloys and Their Structure
- Exhaust Turbine and Jet Propulsion Systems
- The Flow of Gases in Narrow Channels
- A Comparison of the Spanwise Loading Calculated by Various Methods With Experimental Loadings Obtained on a 45 Degree Sweptback Wing of Aspect Ratio 8.02 at a Reynolds Number of 4.0 X 10(6)
- Correction Factors for Wind Tunnels of Elliptic Section With Partly Open and Partly Closed Test Section
- Calculation of the Bending Stresses in Helicopter Rotor Blades
- Critical Velocities of Ultracentrifuges
- Resistance of a Plate in Parallel Flow at Low Reynolds Numbers
- Resonance Sound Absorber With Yielding Wall
- State and Development of Flutter Calculation
- Unstable Capillary Waves on Surface of Separation of Two Viscous Fluids
- The Linearized Characteristics Method and Its Application to Practical Nonlinear Supersonic Problems
- Method of Successive Approximations for the Solution of Certain Problems in Aerodynamics
- Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls With Application to Turbine Blade Cooling
- Theory of Thin-Walled Rods
- Theory of Flame Propagation
- Influence of Static Longitudinal Stability on the Behavior of Airplanes in Gusts
- Stability of the Cylindrical Shell of Variable Curvature
- Concerning the Flow About Ring-Shaped Cowlings Part 6: Further Measurements on Inlet Devices
- Concerning the Flow About Ring-Shaped Cowlings Part 2: Annular Bodies of Infinite Length With Circulation for Smooth Entrance
- Three Papers From Conference On "Wing and Tail-Surface Oscillations: March 6-8, 1941, Munich
- The Structure of Airy's Stress Function in Multiply Connected Regions
- Direct Measurements of Skin Friction
- On Stability and Turbulence of Fluid Flows
- Investigation of Spoiler Ailerons for Use as Speed Brakes or Glide-Path Controls on Two NACA 65-Series Wings Equipped with Full-Span Slotted Flaps
- Generalization of Turbojet and Turbine-Propeller Engine Performance in Windmilling Condition
- Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag
- Basic Differential Equations in General Theory of Elastic Shells
- Torsion and Transverse Bending of Cantilever Plates
- Preliminary Results of a Determination of Temperatures of Flames by Means of K-Band Microwave Attenuation
- A Relation of Wind Shear and Insolation to the Turbulence Encountered by an Airplane in Clear-Air Flight at Low Altitudes
- Experimental Investigation of Forced-Convection Heat-Transfer Characteristics of Lead-Bismuth Eutectic
- Estimation of Neutron Energy for First Resonance From Absorption Cross Section for Thermal Neutrons
- Cooperative Investigation of Relationship Between Static and Fatigue Properties of Heat-Resistant Alloys at Elevated Temperatures
- Plastic Stress-Strain Relations for 75S-T6 Aluminum Alloy Subjected to Biaxial Tensile Stresses
- A Multiple-Range Self-Balancing Thermocouple Potentiometer
- An Investigation of Aircraft Heaters 35: Thermocouple Conduction Error Observed in Measuring Surface Temperatures
- Forced-Convection Heat Transfer to Water at High Pressures and Temperatures in the Nonboiling Region
- Effect of Surface Finish on Fatigue Properties at Elevated Temperatures 1: Low-Carbon N-155 With Grain Size of A.S.T.M. 1
- Preliminary Investigation of Helmholtz Resonators for Damping Pressure Fluctuations in 3.6-Inch Ram Jet at Mach Number 1.90
- Theoretical and Experimental Investigation of Additive Drag
- Thermal Conductivity of 14 Metals and Alloys Up to 1100 Degrees Fahrenheit
- Properties of Low-Carbon N-155 Alloy Bar Stock From 1200 to 1800 Degrees Fahrenheit
- Experimental Investigation of Effect of Jet Exit Configuration on Thrust and Drag
- Altitude Wind Tunnel Investigation of the Performance of Compressor, Combustor, and Turbine Components of Prototype J47D (RX1-1) Turbojet Engine
- An Experimental Study of Water-Pressure Distributions During Landings and Planing of a Heavily Loaded Rectangular Flat-Plate Model
- Comparison of Measured Efficiencies of Nine Turbine Designs with Efficiencies Predicted by Two Empirical Methods
- Effective Modulus in Plastic Buckling of High-Strength Aluminum-Alloy Sheet
- An Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XF3H-1 Airplane: TED No. NACA DE 344