Browse TRAIL Inventories

Recovery temperatures and heat transfer near two-dimensional roughness elements at Mach 3.1

Low-speed yawed-rolling characteristics and other elastic properties of a pair of 40-inch-diameter, 14-ply-rating, type VII aircraft tires

Effects of ground proximity on the thrust of a simple downward-directed jet beneath a flat surface

Effectiveness of boundary-layer control, obtained by blowing over a plain rear flap in combination with a forward slotted flap, in deflecting a slipstream downward for vertical take-off

Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers From 0 to 5

Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines

Experimental Investigation of Effect of Spike- Tip and Cowl-Lip Blunting on the Internal Performance of a Two-Cone Cylindrical-Cowl Inlet at Mach Number 4.95

Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile

Induction System Characteristics and Engine Surge Occurrence for Two Fighter-Type Airplanes

The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes

Correlations Among Ice Measurements, Impingement Rates Icing Conditions, and Drag Coefficients for Unswept NACA 65A004 Airfoil

Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area

The Prospects for Laminar Flow on Hypersonic Airplanes

The Effect of Free-Stream Turbulence on Heat Transfer From a Flat Plate

Area-Suction Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 Degree Swept-Wing Airplane

Some Observations Relating to Recovery of Internal Friction During Fatigue of Aluminum

Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations

Theoretical Performance of Liquid Ammonia With Liquid Oxygen as a Rocket Propellant

Theory and Experiments on Supersonic Air-to-Air Ejectors

Turbulence and Temperature Fluctuations Behind a Heated Grid

Turbulent Shearing Stress in the Boundary Layer of Yawed Flat Plates

A Theoretical Study of Stagnation-Point Ablation

Relative Motion in the Terminal Phase of Interception of a Satellite or a Ballistic Missile

On the Statistical Theory of Turbulence

Relation of Journal Bearing Performance to Minimum Oil-Film Thickness

Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking

Turbulent Flow Through Porous Resistances Slightly Inclined to the Flow Direction

Wall Pressure Fluctuations in a Turbulent Boundary Layer

Wind-Tunnel Investigation at a Mach Number of 2.01 of Forebody Strakes for Improving Directional Stability of Supersonic Aircraft

Two-Dimensional Diffusion Theory Analysis of Reactivity Effects of a Fuel-Plate-Removal Experiment

Comparison of Performance of Two Aerodynamically Similar 14-Inch-Diameter Single-Stage Compressor Rotors of Different Chord Length

Summary of Methods of Measuring Angle of Attack on Aircraft

Low-Temperature, Vapor-Phase Oxidation of Fuel-Rich Hydrocarbon Mixtures

Stall Propagation in a Cascade of Airfoils

Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-Wing Fighter-Bomber-Type Airplane With a Top Inlet at Mach Numbers From 1.6 to 2.35

Study of Hydrogen Embrittlement of Iron by Internal-Friction Methods

Water-Impact Theory for Aircraft Equipped With Nontrimming Hydro-Skis Mounted on Shock Struts

Method of Split Rigidities and Its Application to Various Buckling Problems

Analysis of harmonic forces produced at hub by imbalances in helicopter rotor blades

Lightning Hazards to Aircraft Fuel Tanks

Data From Flow-Field Surveys Behind a Large-Scale Thin Straight Wing of Aspect Ratio 3

Flight Investigation of Effects of Retreating-Blade Stall on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Flight Investigation of Effects of Atmospheric Turbulence and Moderate Maneuvers on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Hydrodynamic Impact Loads on 30 Degree and 60 Degree V-Step Plan-Form Models With and Without Dead Rise

Free-Flight Investigation to Determine the Inlet External Drag of Four Inlet Models at Mach Numbers From 1.50 to 3.00

General Instability of Stiffened Cylinders

Hydrodynamic Impact Loads of a -20 Degree Dead-Rise Inverted-V Model and Comparisons With Loads of a Flat-Bottom Model

Experimental Evaluation of Low-Band-Pass Landing-Gear Shock Absorber for Pulse Loadings

Free-Flight Investigation at Mach Numbers From 0.8 to 1.5 of the Effect of a Fuselage Indentation on the Zero-Lift Drag of a 52.5 Degree Sweptback-Wing-Body Configuration With Symmetrically Mounted Stores on the Fuselage

Prandtl Number Effects on Unsteady Forced-Convection Heat Transfer


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