Browse TRAIL Inventories

The Effect of Wind Bending Deflection on the Rolling Moment Due to Sideslip

A Device for Measuring Sonic Velocity and Compressor Mach Number

Method for Calculation of Pressure Distributions on Thin Conical Bodies of Arbitrary Cross Section in Supersonic Stream

De-Icing Effectiveness of External Electric Heaters for Propeller Blades

Characteristics of Low-Aspect Ratio Wings at Supercritical Mach Numbers

Buckling Tests of Flat Rectangular Plates Under Combined Shear and Longitudinal Compression

Tensile and Compressive Properties of Laminated Plastics at High and Low Temperatures

Effect of Partial Wing Lift in Seaplane Landing Impact

Shear Flows in Multicell Sandwich Sections

Fracture Strength of 75S-T Aluminum Alloy Under Combined Stress

Analytical Method of Determining Transmission of Particles and Radiation Through Great Thickness of Matter

An Improved Photoelastic Method for Determining Plane Stresses

An Investigation of the Low-Speed Static Stability Characteristics of Complete Models Having Sweptback and Sweptforward Wings

Cyclic Engine Test of Cast Vitallium Turbine Buckets 2

Effect of Aerodynamic Hysteresis on Critical Flutter Speed at Stall

Effect of Centrifugal Force on Critical Flutter Speed on a Uniform Cantilever Beam

Efficiency of Radial-Flow Turbine of Turbo Engineering Corporation TTT13-18 Turbosupercharger

Results Obtained During Extension of U.S. Air Force Transonic-Flight Tests of XS-1 Airplane

Indirect Methods for Obtaining Ram-Jet Exhaust-Gas Temperature Applied to Fuel-Metering Control

Wind-Tunnel Investigation of Horizontal Tails 1: Unswept and 35 Degrees Swept-Back Plan Forms of Aspect Ratio 3

High-Speed Aerodynamic Characteristics of a Model Tail Plane with Modified NACA 65-010 Sections and 0 Degree and 45 Degrees Sweepback

High-Speed Aerodynamic Characteristics of a Lateral-Control Model 1: NACA 0012-64 Section with 20-Percent-Chord Plain Aileron and 0 Degree and 45 Degrees Sweepback

The High-Speed Aerodynamic Effects of Modifications to the Wing and Wing-Fuselage Intersection of an Airplane Model with the Wing Swept Back 35 Degrees

High-Speed Stability and Control Characteristics of a Fighter Airplane Model with a Swept-Back Wing and Tail

Relation of Nozzle-Blade and Turbine-Bucket Temperatures to Gas Temperatures in a Turbojet Engine

Theoretical and Experimental Analysis of Low-Drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers of 3.30, 2.75, and 2.45

On the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow

Comparison of Theoretical and Experimental Heat-Transfer Characteristics of Bodies of Revolution at Supersonic Speeds

Prediction of the Effects of Propeller Operation on the Static Longitudinal Stability of Single-Engine Tractor Monoplanes with Flaps Retracted

Method of Estimating the Minimum Size of a Tail or Wing-Tip Parachute for Emergency Spin Recovery of an Airplane

Theoretical Stability Derivatives of Thin Sweptback Wings Tapered to a Point with Sweptback or Sweptforward Trailing Edges for a Limited Range of Supersonic Speeds

Wind-Tunnel Investigation of High-Lift and Stall-Control Devices on a 37 Degree Sweptback Wing of Aspect Ratio 6 at High Reynolds Numbers

Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane

Ditching Tests of Two Models of the Army B-36 Airplane

Ditching Tests of a 1/24-Scale Model of the Lockheed XR60-1 Airplane, TED No. NACA 235

A Restricted List of Aircraft Materials Research Projects

The Method of Characteristics for the Determination of Supersonic Flow Over Bodies of Revolution at Small Angles of Attack

Residual Stress Analysis of Overspeeded Disk With Central Hole by X-Ray Diffraction

One-Dimensional Flows of an Imperfect Diatomic Gas

The Effectiveness at High Speeds of a 10-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section

Experiments on Stability of Bunsen-Burner Flames for Turbulent Flow

The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model

Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer 2: Effect of an Oblique Shock Wave Immediately Ahead of the Inlet

Performance of a Ram-Jet-Type Combustor With Flame Holders Immersed in the Combustion Zone

Note on the Importance of Imperfect-Gas Effects and Variation of Heat Capacities on the Isentropic Flow of Gases

Results Obtained During Accelerated Transonic Tests of the Bell XS-1 Airplane in Flights to a Mach Number of 0.92

A Method for Calculating Flow Fields of Cowlings with Known Surface-Pressure Distributions

Wind-Tunnel Investigation of Horizontal Tails 4: Unswept Plan Form of Aspect Ratio 2 and a Two-Dimensional Model

Effect of High-Lift Devices on the Low-Speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Degrees Sweptback Wing

Wind-Tunnel Investigation of Horizontal Tails 2: Unswept and 35 Degree Swept-Back Plan Forms of Aspect Ratio 4.5


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