TRAIL - Technical Report Archive and Image Library

Effect of Compressor-Outlet Air Bleed on Performance of a Centrifugal-Flow Turbojet Engine with a Constant-Area Jet Nozzle

Some Remarks on an Approximate Method of Estimating the Wave Drag Due to Thickness at Supersonic Speeds of Three-Dimensional Wings With Arbitrary Profile

A Simple Approximate Method for Calculating Spanwise Lift Distributions and Aerodynamic Influence Coefficients

Theoretical Investigation of Velocity Diagrams of a Single-Stage Turbine for a Turbojet Engine at Maximum Thrust Per Square Foot Turbine Frontal Area

A Theoretical Investigation of the Effect of Partial Wing Lift of Hydrodynamic Landing Characteristics of V-Bottom Seaplanes in Step Impacts

Theoretical Performance of an Axial-Flow Compressor in a Gas-Turbine Engine Operating With Inlet Water Injection

Landing-Gear Impact

Experimental Investigation of Eccentricity Ratio, Friction, and Oil Flow of Short Journal Bearings

An Analysis of Supersonic Flow in the Region of the Leading Edge of Curved Airfoils, Including Charts for Determining Surface-Pressure Gradient and Shock-Wave Curvature

Application of Transonic Similarity

A Comparison of Two Methods of Linearized Characteristics for a Simple Unsteady Flow

Two-Dimensional Subsonic Flow Past Elliptic Cylinder by the Variational Method

Use of a Consolidated Porous Medium for Measurement of Flow Rate and Viscosity of Gases at Elevated Pressures and Temperatures

A Method of Selecting the Thickness, Hollowness, and Size of a Supersonic Wing for Least Drag and Sufficient Bending Strength at Specified Flight Conditions

Plastic Stress-Strain Relations for Combined Tension and Compression

An Investigation of Bending-Moment Distribution on a Model Helicopter Rotor Blade and a Comparison With Theory

Derivation of Stability Criterions for Box Beams With Longitudinally Stiffened Covers Connected by Posts

Effects of Cyclic Loading on Mechanical Behavior of 24S-T4 and 75S-T6 Aluminum Alloys and SAE 4130 Steel

Corrections for Drag, Lift, and Moment of an Axially Symmetrical Body Placed in a Supersonic Tunnel Having a Two-Dimensional Pressure Gradient

A Description and a Comparison of Certain Nonlinear Curve-Fitting Techniques, With Applications to the Analysis of Transient-Response Data

A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial-, Radial-, and Mixed-Flow Types

Implication of the Transport Equation for the Semiempirical Treatment of Shields

Preview of Behavior of Grain Boundaries in Creep of Aluminum Bicrystals

Summary of Available Hail Literature and the Effect of Hail on Aircraft in Flight

Influence of Nonmartensitic Transformation Products on Mechanical Properties of Tempered Martensite

Radiant-Interchange Configuration Factors

The Stability Under Longitudinal Compression of Flat Symmetric Corrugated-Core Sandwich Plates With Simply Supported Loaded Edges and Simply Supported or Clamped Unloaded Edges

Approximate Theory for Calculation of Lift of Bodies, Afterbodies, and Combinations of Bodies

Method for Calculation of Compressible Laminar Boundary-Layer Characteristics in Axial Pressure Gradient With Zero Heat Transfer

A Study of the Stability of the Laminar Boundary Layer as Affected by Changes in the Boundary-Layer Thickness in Regions of Pressure Gradient and Flow Through the Surface

Stress Problems in Pressurized Cabins

Stresses and Deformations in Wings Subjected to Torsion

Coincidence Method Applied to Ion Beam Measurement

Matrix and Relaxation Solutions That Determine Subsonic Through Flow in an Axial-Flow Gas Turbine

Theoretical and Experimental Analysis of One-Dimensional Compressible Flow in a Rotating Radial-Inlet Impeller Channel

Experimental Investigation of the Turbulent-Boundary-Layer Temperature-Recovery Factor on Bodies of Revolution at Mach Numbers From 2.0 to 3.8

Electrical Pressure Integrator

Influence of Chemical Composition on Rupture Test Properties at 1500 Degrees Fahrenheit of Forged Chromium-Cobalt-Nickel-Iron Base Alloys

On the Form of the Turbulent Skin-Friction Law and Its Extension to Compressible Flows

Theoretical Distribution of Slip Angles in an Aggregate of Face-Centered Cubic Crystals

The Application of Planing Characteristics to the Calculation of the Water-Landing Loads and Motions of Seaplanes of Arbitrary Constant Cross Section

Water-Pressure Distribution During Landings of a Prismatic Model Having an Angle of Dead Rise of 22 1/2 Degrees and Beam-Loading Coefficients of 0.48 and 0.97

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

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