TRAIL - Technical Report Archive and Image Library

An Approximate Solution for Axially Symmetric Flow Over a Cone With an Attached Shock Wave

Some Measurements of Time and Space Correlation in Wind Tunnel

Interaction of a Free Flame Front With a Turbulence Field

Nonlifting Wing-Body Combinations With Certain Geometric Restraints Having Minimum Wave Drag at Low Supersonic Speeds

On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression

Optimum Flight Paths of Turbojet Aircraft

Steady Properly-Banked Turns of Turbojet-Propelled Airplanes

A Method of Quadrature for Calculation of the Laminar and Turbulent Boundary Layer in Case of Plane and Rotationally Symmetrical Flow

General Solutions of Optimum Problems in Nonstationary Flight

Incompressible Flutter Characteristics of Representative Aircraft Wings

Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure

Theory of Dynamic Creep

Theory of Reversible and Nonreversible Cracks in Solids

Influence of Alloying upon Grain-Boundary Creep

Metallography of Aluminum and Its Alloys: Use of Electrolytic Polishing

Influence of Hot-Working Conditions on High-Temperature Properties of a Heat-Resistant Alloy

Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds

Contributions on the Mechanics of Boundary-Layer Transition

Charts for Estimating Performance of High-Performance Helicopters

Characteristics of Turbulence in Boundary Layer with Zero Pressure Gradient

Some Results of Flight Testing of Ski-Equipped Aircraft at the Naval Air Test Center

Investigation of a Cermet Gas-Turbine-Blade Material of Titanium Carbide Infiltrated With Hastalloy C

Study of Effects of Microstructure and Anisotropy on Fatigue of 23S-T4 Aluminum Alloy

Application of Stream-Filament Techniques to Design of Diffuser Between Compressor and Combustor in a Gas-Turbine Engine

Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

The Effect of a 4-Percent-High Spoiler on Buffeting Forces on a NACA 65(Sub 06)A004 Two-Dimensional Airfoil at Subsonic Mach Numbers

Effects of Wing Position and Fuselage Size on the Low-Speed Static Rolling Stability Characteristics of a Delta-Wing Model

Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips

Free-Flight Tests to Determine the Power-on and Power-Off Pressure Distribution and Drag of the NACA RM-10 Research Vehicle at Large Reynolds Numbers Between Mach Numbers 0.8 and 3.0

Theoretical Calculations of the Pressures, Forces, and Moments Due to Various Lateral Motions Acting on Thin Isolated Vertical Tails With Supersonic Leading and Trailing Edges

Investigation of the Effects of an Airfoil Section Modification on the Aerodynamic Characteristics at Subsonic and Supersonic Speeds of a Thin Swept Wing of Aspect Ratio 3 in Combination With a Body

Thermal Analysis of Sodium Hydroxide Containing the Reaction Products of Sodium Hydroxide and Chromium Metal

Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine 3: Curved-Root Design

Meteorological Problems Associated With Commercial Turbojet-Aircraft Operation

A Method for Determining the Composition of Methanol-Trimethyl Borate Mixtures

Summary of the Flight Conditions and Maneuvers in Which Maximum Wing and Tail Loads Were Experienced on a Swept-Wing Fighter Airplane

A Theoretical Analysis of a Simple Aerodynamic Device to Improve the Longitudinal Damping of a Cruciform Missile Configuration at Supersonic Speeds

Effect of Taper Ratio on Lift, Drag, and Pitching-Moment Characteristics of Thin Wings of Aspect Ratio 3 With 53.1 Degrees Sweepback of Leading Edge at Subsonic and Supersonic Speeds

A Simplified Method for Calculating Aeroelastic Effects on the Roll of Aircraft

Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes

Comparison of the Static Stability of a 68.7 Degree Delta-Wing Model with Dihedral and a Twisted and Cambered Wing Model of the Same Plan Form

Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing

Effect of Dissolved Oxygen on the Filterability of Jet Fuels for Temperatures Between 300 Degrees and 400 Degrees Fahrenheit

Note on Hovering Turns with Tandem Helicopters

Effects of Wing-Mounted Tank-Type Stores on the Low Lift Buffeting and Drag of a Swept-Wing Airplane Configuration Between Mach Numbers of 0.8 and 1.3

Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane

Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

Experimental Investigation of a 0.4 Hub-Tip Diameter Ratio Axial-Flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers 2: Stage and Blade-Element Performance

Investigation of Two Short Annular Diffuser Configurations Utilizing Section and Injection as a Means of Boundary-Layer Control

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