Browse TRAIL Inventories

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

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

Minimum Ignition of Six Pure Hydrocarbon Fuels of the C₂ and C₆ Series

An Investigation of Longitudinal Control Characteristics of a Wing-Tip Control Surface on a Sweptback Wing at Transonic Speeds by the NACA Wing-Flow Method

Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range

Investigation of an NACA 4-(5)(05)-041 Four-Blade Propeller With Several Spinners at Mach Numbers Up to 0.90

Flight Investigation From Mach Number 0.8 to 2.0 to Determine Some Effects of Wing-to-Tail Distance on the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing-Canard Missile

Flight Measurements at Mach Numbers From 1.1 to 1.9 of the Zero-Lift Drag of a Twin-Engine Supersonic Ram-Jet Configuration

Handling Qualities of High-Speed Airplanes

Hydrodynamic Directional Behavior of a Swept Planing-Tail Hull


Published Year

Subject

Author

‹‹ previous 1 2 ... 40 41 42 43 44 45 46 ... 143 144 next ››