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- Equal-Strength Design of Tension-Field Webs and Uprights
- Theory of Supersonic Potential Flow in Turbomachines
- Fatigue and Static Tests of Flush-Riveted Joints
- Direct Measurements of Skin Friction
- Effect of High-Lift Devices on the Low-Speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Degrees Sweptback Wing
- Hydrodynamic Characteristics of a Low-Drag, Planing-Tail Flying Boat Hull
- Supersonic Conical Flow
- Laminar Boundary Layer Over Flat Plate in a Flow Having Circular Streamlines
- Normal Accelerations and Operating Conditions Encountered by a Helicopter in Air-Mail Operations
- 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
- 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