Browse TRAIL Inventories

An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control

Some Effects of Vanes and of Turbulence in Two-Dimensional Wide-Angle Subsonic Diffusers

Lag in Pressure Systems at Extremely Low Pressures

Method for Determining the Need to Rework or Replace Compressor Rotor Blades Damaged by Foreign Objects

An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations

Use of Short Flat Vanes for Producing Efficient Wide-Angle Two-Dimensional Subsonic Diffusers

Effect of Dissociation on Exhaust-Nozzle Performance

Discrete Potential Theory for Two-Dimensional Laplace and Poisson Difference Equations

Approximate Method for Calculation of Laminar Boundary Layer With Heat Transfer on a Cone at Large Angle of Attack in Supersonic Flow

Free-Flight Investigation to Determine the Drag of Flat- and Vee- Windshield Canopies on a Parabolic Fuselage With and Without Transonic Indentation Between Mach Numbers of 0.75 and 1.35

Charts Relating the Compressive and Shear Buckling Stresses of Longitudinally Supported Plates to the Effective Deflectional Stiffness

Performance of a Two-Dimensional Cascade Inlet at a Free-Stream Mach Number of 3.05 and at Angles of Attack of -3 Degrees, 0 Degrees, 3 Degrees, and 6 Degrees

Effects of Canard Surface Size on Stability and Control Characteristics of Two Canard Airplane Configuration at Mach Numbers of 1.41 and 2.01

Handbook of Structural Stability Part 6: Strength of Stiffened Curved Plates and Shells

High-Speed Hydrodynamic Characteristics of a Flat Plate and 20 Degrees Dead-Rise Surface in Unsymmetrical Planing Conditions

Mass Transfer Cooling Near the Stagnation Point

On Pairs of Solutions of a Class of Internal Viscous Flow Problems With Body Forces

Ground Simulator Studies of a Small Side-Located Controller in a Power Control System

Turbojet Engine Noise Reduction With Mixing Nozzle-Ejector Combinations

Experimental Investigation of the Effect of Circumferential Inlet Flow Distortion on the Performance of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages

Static Longitudinal and Lateral Stability Characteristics at Low Speed of 60 Degree Sweptback-Midwing Models Having Wings with an Aspect Ratio of 2, 4, or 6

Effect of Some External Crosswise Stiffeners on the Heat Transfer and Pressure Distribution on a Flat Plate at Mach Numbers of 0.77, 1.39, and 1.98

Compressive Strength and Creep of 17-7 PH Stainless-Steel Plates at Elevated Temperatures

Second-Order Slender-Body Theory: Axisymmetric Flow

Experimental Lift-Drag Ratios for Two Families of Wing-Body Combinations at Supersonic Speeds

Transient Heating Effects on the Bending Strength of Integral Aluminum-Alloy Box Beams

Effect of Temperature on Dynamic Modulus of Elasticity of Some Structural Alloys

Measurements in a Shock Tube of Heat-Transfer Rates at the Stagnation Point of a 1.0-Inch-Diameter Sphere for Real-Gas Temperatures Up to 7,900 R

An Approximate Method for Design or Analysis of Two-Dimensional Subsonic-Flow Passages

Flight Investigation of a Full-Scale Aircraft Ejector with Various Spacing Ratios and Correlation with Small-Scale Tests

Simulator Investigation of Command Reaction Controls

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

A Simulator Investigation of Factors Affecting the Design and Utilization of a Stick Pusher for the Prevention of Airplane Pitch-Up

Lift and Moment on Thin Arrowhead Wings with Supersonic Edges Oscillating in Symmetric Flapping and Roll and Application to the Flutter of an All-Moveable Control Surface

Tables and Graphs of Normal-Shock Parameters at Hypersonic Mach Numbers and Selected Altitudes

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


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