Browse TRAIL Inventories

Effect of Advance Ratio on Flight Performance of a Modified Supersonic Propeller

On Fully Developed Channel Flows: Some Solutions and Limitations, and Effects of Compressibility, Variable Properties, and Body Forces

Experimental Investigation of Distortion Removal Characteristics of Several Free-Wheeling Fans

Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives

Some Static Longitudinal Stability Characteristics of an Overlapped-Type Tandem-Rotor Helicopter at Low Airspeeds

Reflection and Transmission of Sound by a Slotted Wall Separating Two Moving Fluid Streams

Investigation of the Performance and Internal Flow of a Variable-Area, Variable-Internal-Contraction Inlet at Mach Numbers of 2.00, 2.50, and 2.92

Transonic Wind-Tunnel Investigation of the Effect of Horizontal Tail on Longitudinal Stability of Two 60 Degree Sweptback-Wing-Body Configurations with Aspect Ratios of 2.67 and 4.00

Temperature-Pressure-Time Relations in a Closed Cryogenic Container

Flight Measurements of the Vibratory Stresses on a Propeller Designed for an Advance Ratio of 4.0 and a Mach Number of 0.82

Flight Measurements of the Vibratory Bending and Torsional Stresses on a Modified Supersonic Propeller for Forward Mach Numbers up to 0.95

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

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components

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

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

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

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

Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile

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


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