TRAIL - Technical Report Archive and Image Library

A General Integral Form of the Boundary-Layer Equation for Incompressible Flow With an Application to the Calculation of the Separation Point of Turbulent Boundary Layers

The External-Shock Drag of Supersonic Inlets Having Subsonic Entrance Flow

Preliminary Investigation of Reflections of Oblique Waves from a Porous Wall

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine: 1: Rotor Blades With 10 Tubes in Cooling-Air Passages

Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds: Tail Attached to a Segment of the Foreshortened Body

Wind-Tunnel Investigation of a 1/6-Scale Model of the Bumblebee XPM Missile at High Subsonic Speeds

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 2: Rotor Blades With 15 Fins in Cooling-Air Passages

Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails

Investigation of Power Requirements for Ice Prevention and Cyclical De-Icing of Inlet Guide Vanes with Internal Electric Heaters

Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis

Photomicrographic Investigation of Spontaneous Freezing Temperatures of Supercooled Water Droplets

The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment

Investigation of Aerodynamic and Icing Characteristics of Water-Inertia-Separation Inlets for Turbojet Engines

Improvements in Heat Transfer for Anti-Icing of Gas-Heated Airfoils with Internal Fins and Partitions

Blockage Corrections for Three-Dimensional-Flow Closed-Throat Wind Tunnels, with Consideration of the Effect of Compressibility

Flight investigation of the effect of transient wing response on measured accelerations of a modern transport airplane in rough air

Prandtl-Meyer Flow for a Diatomic Gas of Variable Specific Heat

Tables for Determining Reduction of Energy and Intensity of X-Rays and Gamma-Rays at Various Scattering Angles in Small Thickness of Matter

A Review of Information on the Mechanical Properties of Aluminum Alloys at Low Temperatures

Water Landing Investigation of a Model Having a Heavy Beam Loading and a 30 Degree Angle of Dead Rise

Investigation of a Two-Step Nozzle in the Langley 11-Inch Hypersonic Tunnel

A Theoretical Investigation of the Effect on the Lateral Oscillations of an Airplane of an Automatic Control Sensitive to Yawing Accelerations

Effect of Humidity on Performance of Turbojet Engines

Effect of Heat-Capacity Lag on the Flow Through Oblique Shock Waves

Bonding Investigation of Titanium Carbide With Various Elements

Analytical Method for Determining Transmission and Absorption of Time-Dependent Radiation Through Thick Absorbers 3: Absorber With Radioactive Daughter Products

An Investigation of the Effect of Tetraethyl Lead and Ethyl Nitrite on the Autoignition Characteristics of Isooctane and Triptane

Knock-Limited Performance of Fuel Blends Containing Ethers

Method for Determining Pressure Drop of Air Flowing Through Constant-Area Passages for Arbitrary Heat-Input Distributions

Linearized Supersonic Theory of Conical Wings

Effect of Initial Mixture Temperature on Flame Speeds and Blow-Off Limits of Propane - Air Flames

Hovering and Low-Speed Performance and Control Characteristics of an Aerodynamic-Servocontrolled Helicopter Rotor System as Determined on the Langley Helicopter Tower

Shear Stress Distribution Along Glue Line Between Skin and Cap-Strip of an Aircraft Wing

Free Oscillations of an Atmosphere in Which Temperature Increases Linearly With Height

Strength Properties of Rayon-Mat Honeycomb Core Materials

Analysis of V-g data obtained from several naval airplanes

Planing Characteristics of Six Surfaces Representative of Hydro-Ski Forms

Performance of Three High-Recovery-Factor Thermocouple Probes for Room-Temperature Operation

A Preliminary Experimental and Analytical Evaluation of Diborane as a Ram-Jet Fuel

Preliminary Investigation of a Submerged Air Scoop Utilizing Boundary-Layer Suction to Obtain Increased Pressure Recovery

Exploratory Investigation of Leading-Edge Chord-Extensions to Improve the Longitudinal Stability Characteristics of Two 52 Degree Sweptback Wings

Flight Investigation at Mach Numbers From 0.8 to 1.4 to Determine the Zero-Lift Drag of Wings With 'M' and 'W' Plan Forms

Experimental Investigation of Various Wing-Mounted External Stores on a Wing-Fuselage Combination Having a Sweptback Wing of Inverse Taper Ratio

Experimental Investigation of Various External-Store Configurations on a Model of a Tailless Airplane With a Sweptback Wing

An Experimental Investigation at Large Scale of an NACA Submerged Intake and Deflector Installation on the Rearward Portion of a Fuselage

Some Effects of Chordwise Fences on the Aerodynamic Characteristics of Four Moderately Sweptback Wings in the Low-Lift Range at Transonic Mach Numbers and at Mach Number 1.9

Keyword Search

Published Year

Subject

Author