Browse TRAIL Inventories

Drag Tests of an NACA 65(215)-114, a = 1.0 Practical-Construction Airfoil Section Equipped with a 0.295-Airfoil-Chord Slotted Flap

Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 75S-T Sheet

Lifting-Surface-Theory Aspect-Ratio Corrections to the Lift and Hinge-Moment Parameters for Full-Span Elevators on Horizontal Tail Surfaces

A Metallurgical Investigation of Large Forged Discs of Low-Carbon N-155 Alloy

A Study of Piston-Ring Friction

Performance Tests of Wire Strain Gages 5: Error in Indicated Bending Strains in Thin Sheet Metal Due to Thickness and Rigidity of Gage

Experimental Studies of the Knock-Limited Blending Characteristics of Aviation Fuels 2: Investigation of Leaded Paraffinic Fuels in an Air-Cooled Cylinder

Effect of Geometric Dihedral on the Aerodynamic Characteristics of Two Isolated Vee-Tail Surfaces

The Spot Welding of Dissimilar Aluminum Alloys in the 0.040-Inch Thickness

The Spot Welding of Alclad 24S-T in Thicknesses of 0.064, 0.081, and 0.102 Inch

A Study of Several Parameters Controlling the Trajectories of a Supersonic Antiaircraft Missile Powered With Solid- or Liquid-Fuel Rockets

The Linear Perturbation Theory of Axially Symmetric Compressible Flow With Application to the Effect of Compressibility on the Pressure Coefficient at the Surface of a Body of Revolution

General Treatment of Compressible Flow in Ejectors and Example of Its Application to Problem of Effect of Ejector Addition on Thrust of Jet-Propulsion Units

Flight Investigation of Thrust Augmentation of a Turbojet Engine by Water-Alcohol Injection

Preliminary Investigation of Effects of Gamma Radiation on Age-Hardening Rate of an Aluminum-Copper Alloy

The Subsonic Aerodynamic Characteristics of Two Double-Wedge Airfoil Sections Suitable for Supersonic Flight

Estimation of Range of Stability Derivatives for Current and Future Pilotless Aircraft

A Device for Measuring Sonic Velocity and Compressor Mach Number

Tests of Submerged Duct Installation on a Modified Airplane in the Ames 40- by 80-foot Wind Tunnel

Estimate of Hull-Weight Change with Varying Length-Beam Ratio for Flying Boats

Effect of Modifications to Induction System on Altitude Performance of V-1710-93 Engine 3: Use of Parabolic Rotating Guide Vanes and NACA Designed Auxiliary-Stage Inlet Elbow and Interstage Duct

Frequency-Response Method for Determination of Dynamic Stability Characteristics of Airplanes With Automatic Controls

Flight Investigation on a Fighter-Type Airplane of Factors Which Affect the Loads and Load Distributions on the Vertical Tail Surfaces During Rudder Kicks and Fishtails

A Theoretical Investigation of Hydrodynamic Impact Loads on Scalloped-Bottom Seaplanes and Comparisons With Experiment

Dislocation Theory of the Fatigue of Metals

Coefficient of Friction, Oil Flow and Heat Balance of a Full-Journal Bearing

Spark-Timing Control Based on Correlation of Maximum-Economy Spark Timing, Flame-Front Travel, and Cylinder-Pressure Rise

On Similarity Rules for Transonic Flows

The Development of Jet-Engine Nacelles for a High-Speed Bomber Design

Calculations and Experimental Investigations on the Feed-Power Requirement of Airplanes With Boundary-Layer Control

Analytical Treatment of Normal Condensation Shock

Calibration and Measurement in Turbulence Research by the Hot-Wire Method

The Combination of Internal-Combustion Engine and Gas Turbine

Description of Russian Aircraft Engines "AM 35" and "AM 38"

Development and Construction of an Interferometer for Optical Measurements of Density Fields

Determination of the Stress Concentration Factor of a Stepped Shaft Stressed in Torsion by Means of Precision Strain Gages

Concerning the Velocity of Evaporation of Small Droplets in a Gas Atmosphere

Compressible Flow Tables for Air

Cones in Supersonic Flow

Compression Shocks of Detached Flow

The Distribution of Loads on Rivets Connecting a Plate to a Beam Under Transverse Loads

Drag Reduction by Suction of the Boundary Layer Separated Behind Shock Wave Formation at High Mach Numbers

Force and Pressure-Distribution Measurements on a Rectangular Wing With a Slotted Droop Nose and With Either Plain and Split Flaps in Combination or a Slotted Flap

Investigations on Reductions of Friction on Wings, in Particular by Means of Boundary Layer Suction

NACA Conference on Aerodynamic Problems of Transonic Airplane Design

A Method for Estimating Heat Requirements for Ice Prevention Gas Heated Hollow Propeller Blades

Introduction to the Problem of Rocket-Powered Aircraft Performance

Wind-tunnel investigation of the effect of tab balance on tab and control-surface characteristics

The Performance of a Composite Engine Consisting of a Reciprocating Spark-Ignition Engine, a Blow-Down Turbine, and a Steady-Flow Turbine

Experimental Studies of Knock-Limited Blending Characteristics of Aviation Fuels 3 - Aromatics and Cycloparaffins


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