TRAIL - Technical Report Archive and Image Library

A Theoretical and Experimental Investigation of the Effects of Yaw on Pressures, Forces, and Moments During Seaplane Landings and Planing

Practical Calculation of Second-Order Supersonic Flow Past Nonlifting Bodies of Revolution

High-Speed Subsonic Characteristics of 16 NACA 6-Series Airfoil Sections

Method and Graphs for the Evaluation of Air-Induction Systems

Simulation of Linearized Dynamics of Gas-Turbine Engines

Second Approximation to Laminar Compressible Boundary Layer on Flat Plate in Slip Flow

An Extension of Lifting Rotor Theory to Cover Operation at Large Angles of Attack and High Inflow Conditions

Driving Standing Waves by Heat Addition

Choking of a Subsonic Induction Tunnel by the Flow from an Induction Nozzle

Equivalent-Plate Theory for a Straight Multicell Wing

On the Application of Transonic Similarity Rules

An Analysis of Laminar Free-Convection Flow and Heat Transfer About a Flat Plate Parallel to the Direction of the Generating Body Force

Introduction to Electrical-Circuit Analogies for Beam Analysis

A Simple Numerical Method for the Calculation of the Laminar Boundary Layer

Transition Caused by the Laminar Flow Separation

Friction and Wear

The Excitation of Unstable Perturbations in a Laminar Friction Layer

Wind-Tunnel Corrections at High Subsonic Speeds Particularly for an Enclosed Circular Tunnel

Calculation of the Lateral-Dynamic Stability of Aircraft

Comparison of Turbojet-Engine Altitude Performance Characteristics and Ignition Limits With MIL-F-5624A Fuel, Grades JP-3 and JP-4

Investigations of the Boundary-Layer Control on a Full Scale Swept Wing With Air Bled Off From the Turbojet

Development of a Laminar Boundary Layer Behind a Suction Point

Generalized Theory for Seaplane Impact

Theory and Procedure for Determining Loads and Motions in Chine-Immersed Hydrodynamic Impacts of Prismatic Bodies

Concerning the Flow About Ring-Shaped Cowlings of Finite Thickness: Part 1

Concerning the Flow About Ring-Shaped Cowlings Part 8: Further Measurements on Annular Profiles

On a Solution of the Nonlinear Differential Equation for Transonic Flow Past a Wave-Shaped Wall

Extension to the Cases of Two Dimensional and Spherically Symmetric Flows of Two Particular Solutions to the Equations of Motion Governing Unsteady Flow in a Gas

The Structure of Turbulence in Fully Developed Pipe Flow

On the Development of Turbulent Wakes From Vortex Streets

An Experimental Investigation of Transonic Flow Past Two-Dimensional Wedge and Circular-Arc Sections Using a Mach-Zehnder Interferometer

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

Experimental Determination of the Effect of Horizontal-Tail Size, Tail Length, and Vertical Location on Low-Speed Static Longitudinal Stability and Damping Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces

An Iterative Transformation Procedure for Numerical Solution of Flutter and Similar Characteristics-Value Problems

Experimental Aerodynamic Derivatives of a Sinusoidally Oscillating Airfoil in Two-Dimensional Flow

Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Method of Positioning the Radar Antenna on the Speed of Response

Theoretical Investigation of the Stability at Negative Static Margins of a Supersonic Missile With an Autopilot Sensitive to Pitch Angle and Pitching Velocity

The Normal Component of the Induced Velocity in the Vicinity of a Lifting Rotor and Some Examples of Its Application

Preliminary Investigation of a New Type of Supersonic Inlet

The Ames Supersonic Free-Flight Wind Tunnel

Supplementary Bibliography of NACA Reports Related to Instrumentation and Research Techniques

Performance Characteristics of a Normal-Shock Side Inlet Located Downstream of a Canard Control Surface at Mach Numbers of 1.5 and 1.8

A Method for Estimating Speed Response of Gas-Turbine Engines

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 12: Cooling Effectiveness of a Blade With an Insert and With Fins Made of a Continuous Corrugated Sheet

An Investigation at Subsonic Speeds of the Rolling Effectiveness of a Small Perforated Spoiler on a Wing Having 45 Degrees of Sweepback

Dynamic Response of Turbine-Blade Temperature to Exhaust-Gas Temperature for Gas-Turbine Engines

Experimental Investigation of Axial-Flow Compressor Stator Blades Designed to Obtain High Turning Angles by Means of Boundary-Layer Suction

Use of Fences to Increase Uniformity of Boundary Layer on Side Walls of Supersonic Wind Tunnels

Radiant Heat Transfer From Flames in a Single Tubular Turbojet Combustor

Some Dynamic Characteristics of a Turbojet Engine for Large Accelerations

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