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- Effects of Several Arrangements of Rectangular Vortex Generators on the Static-Pressure Rise Through a Short 2:1 Diffuser
- Effects of Design Details on the Fatigue Strength of 355-T6 Sand-Cast Aluminum Alloy
- Evaluation of High-Angle Attack Aerodynamic-Derivative Data and Stall-Flutter Prediction Techniques
- Experimental Pressure Distributions Over Two Wing-Body Combinations at Mach Number 1.9
- Power Unit for High-Intensity Light Source
- Mechanical and Corrosion Tests of Spot-Welded Aluminum Alloys
- Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-Percent-Thick, Biconvex Section
- Preliminary Investigation of the Control of a Gas-Turbine Engine for a Helicopter
- The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45 Degrees of Sweepback, an Aspect Ratio of 3, and a Taper Ratio of 0.5
- Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield
- Combustion-Chamber Performance Characteristics of a Python Turbine-Propeller Engine Investigated in Altitude Wind Tunnel
- Sideslip in a Viscous Compressible Gas
- Lateral Control by Spoilers at the DVL
- On the Problem of Gas Flow Over an Infinite Cascade Using Chaplygin's Approximation
- On the Theory of Thin and Thin-Walled Rods
- 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