TRAIL - Technical Report Archive and Image Library

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

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

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

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

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

Wind-Tunnel Investigation of the Descent Characteristics of Bodies of Revolution Simulating Anti-Personnel Bombs

Experimental Values of the Surface Tension of Supercooled Water

An Empirical Method Permitting Rapid Determination of the Area, Rate and Distribution of Water-Drop Impingement on an Airfoil of Arbitrary Section at Subsonic Speeds

Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors

Determination of Shapes of Boattail Bodies of Revolution for Minimum Wave Drag

Lateral-Control Characteristics and Dihedral Effect of a Wing-Body Combination With a Variable-Incidence Triangular Wing and Wing-Tip Ailerons at a Mach Number of 1.52

NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations

Method for Estimating Lift Interference of Wing-Body Combinations at Supersonic Speeds

Calculated Performance of a Mercury-Compressor-Jet Powered Airplane Using a Nuclear Reactor as an Energy Source

Analysis of Meteorological Data Obtained During Flight in a Supercooled Stratiform Cloud of High Liquid-Water Content

Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds

An Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XF3H-1 Airplane

Meteorological Analysis of Icing Conditions Encountered in Low-Altitude Stratiform Clouds

A General Correlation of Temperature Profiles Downstream of a Heated-Air Jet Directed Perpendicularly to an Air Stream

Analysis of the Liquid-Metal Turbojet Cycle for Propulsion of Nuclear Powered Aircraft

Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations

Possible Application of Blade Boundary-Layer Control to Improvement of Design and Off-Design Performance of Axial-Flow Turbomachines

Practical Methods of Calculation Involved in the Experimental Study of an Autopilot and the Autopilot-Aircraft Combination

A Photoelastic Investigation of Stress Concentrations Due to Small Fillets and Grooves in Tension

Torsional Strength of Stiffened D-Tubes

Turbulence-Intensity Measurements in a Jet of Air Issuing From a Long Tube

Water-Landing Investigation of a Model Having Heavy Beam Loadings and 0 Degrees Angle of Dead Rise

Flow Separation Ahead of Blunt Bodies at Supersonic Speeds

An Investigation by the Hodograph Method of Flow Through a Symmetrical Nozzle With Locally Supersonic Regions

Experimental Investigation of Localized Regions of Laminar-Boundary-Layer Separation

An Investigation of Aircraft Heaters 37: Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promotors

An Investigation of Aircraft Heaters 34: Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Between a Flat and a Wave-Shaped Plate

An investigation of aircraft heaters 36: preliminary investigation of a combustion-type aircraft heater

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