Browse TRAIL Inventories

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

Preliminary Investigation of Cooling-Air Ejector Performance at Pressure Ratios from 1 to 10

Stability and Control Measurements Obtained during USAF-NACA Cooperative Flight-Test Program on the X-4 Airplane (USAF No. 46-677)

Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the McDonnell F2H-3 Airplane

Free-Spinning-Tunnel Investigation to Determine the Effect of Two Nose Designs on Spin and Recovery Characteristics of a 1/20-Scale Model of the McDonnel XF3H-1 Airplane: TED No. NACA DE 343

Low-Speed Characteristics of a 45 Degree Swept Wing with Leading-Edge Inlets

Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag

Analytical Investigation of Fully Developed Laminar Flow in Tubes With Heat Transfer With Fluid Properties Variable Along the Radius

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

Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield

A Summary of Meteorological Conditions Associated With Aircraft Icing and a Proposed Method of Selecting Design Criterions for Ice-Protection Equipment

Study of Chromium-Frit-Type Coatings for High-Temperature Protection of Molybdenum

Comparison of Heat Transfer from Airfoil in Natural and Simulated Icing Conditions


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