TRAIL - Technical Report Archive and Image Library

Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01

Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle

Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359

The Low-Speed Lift and Drag Characteristics of a Series of Airplane Models Having Triangular or Modified Triangular Wings

Damping in Pitch of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds

Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01

Effects of External Store Mounting on the Buffet, Trim, and Drag Characteristics of Rocket-Powered Fuselage and Store Combinations Between Mach Numbers of 0.7 and 1.4

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 13: Endurance Evaluation of Several Protective Coatings Applied to Turbine Blades of Nonstrategic Steels

Effects of Span and Spanwise and Chordwise Location on the Control Effectiveness of Spoilers on a 50 Degree Sweptback Wing at Mach Numbers of 1.41 and 1.96

Effect of Type of Porous Surface and Suction Velocity Distribution on the Characteristics of a 10.5 Percent-Thick Airfoil With Area Suction

A Small Pirani Gage for Measurements of Nonsteady Low Pressures

Theoretical Investigation of the Supersonic Lift and Drag of Thin, Sweptback Wings With Increased Sweep Near the Root

A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip

The Drag of Finite-Length Cylinders Determined From Flight Tests at High Reynolds Numbers for a Mach Number Range From 0.5 to 1.3

Estimation of Hydrodynamic Impact Loads and Pressure Distributions on Bodies Approximating Elliptical Cylinders With Special Reference to Water Landings of Helicopters

Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-Alloy Hand Forgings

Calculation and Measurement of Normal Modes of Vibration of an Aluminum-Alloy Box Beam With and Without Large Discontinuities

Application of Silver Chloride in Investigations of Elasto-Plastic States of Stress

Column Strength of H-Sections and Square Tubes in Postbuckling Range of Component Plates

An Investigation of the Experimental Aerodynamic Loading on a Model Helicopter Rotor Blade

Effects of Parallel-Jet Mixing on Downstream Mach Number and Stagnation Pressure With Application to Engine Testing in Supersonic Tunnels

Investigation of the Statistical Nature of the Fatigue of Metals

The Creep of Single Crystals of Aluminum

Subsonic Flow of Air Through a Single-Stage and a Seven-Stage Compressor

Influence of Rotor-Engine Torsional Oscillation on Control of Gas-Turbine Engine Geared to Helicopter Rotor

A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness

A Study of the Stability of the Incompressible Laminar Boundary Layer on Infinite Wedges

A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes

The Structure of Turbulence in Fully Developed Pipe Flow

A Digital Automatic Multiple Pressure Recorder

Reflection of a Weak Shock Wave From a Boundary Layer Along a Flat Plate 1: Interaction of Weak Shock Waves With Laminar and Turbulent Boundary Layers Analyzed by Momentum-Integral Method

Reflection of Weak Shock Wave From a Boundary Layer Along a Flat Plate 2: Interaction of Oblique Shock Wave With a Laminar Boundary Layer Analyzed by Differential-Equation Method

The Galvanic Corrosion Theory for Adherence of Porcelain-Enamel Ground Coats to Steel

Relation Between Roughness of Interface and Adherence of Porcelain Enamel to Steel

Appraisal of Hazards to Human Survival in Airplane Crash Fires

Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects

Estimation of Forces and Moments Due to Rolling for Several Slender-Tail Configurations at Supersonic Speeds

A Rapid Method for Use in Design of Turbines Within Specified Aerodynamic Limits

Flow Properties of Strong Shock Waves in Xenon Gas as Determined for Thermal Equilibrium Conditions

Counting Methods and Equipment for Mean-Value Measurements in Turbulence Research

Deflection of Delta Wings Having a Carry-Through-Bay Chord Smaller than the Wing Root Chord

The Effects of Camber on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-Percent-Thick Modified NACA Four-Digit-Series Airfoil Section

Analysis of Multicell Delta Wings on Cal-Tech Analog Computer

An Analytical Investigation of the Effect of the Rate of Increase of Turbulent Kinetic Energy in the Stream Direction on the Development of Turbulent Boundary Layers in Adverse Pressure Gradients

The Condensation Line of Air and the Heats of Vaporization of Oxygen and Nitrogen

Some Problems on the Theory of Creep

A New Simple Interferometer for Obtaining Quantitatively Evaluable Flow Patterns

Keyword Search

Published Year

Subject

Author