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- Discrepancies Between Theoretical and Observed Behavior of Cyclically Loaded Bearings
- The Hydrodynamic Lubrication of Cyclically Loaded Bearings
- A Study of Second-Order Supersonic-Flow Theory
- Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds
- Estimation of Low-Speed Lift and Hinge-Moment Parameters for Full-Span Trailing-Edge Flaps on Lifting Surfaces With and Without Sweepback
- Flexural Fatigue Strengths of Riveted Box Beams - Alclad 14S-T6, Alclad 75S-T6, and Various Tempers of Alclad 24S
- Mathematical Improvement of Method for Computing Poisson Integrals Involved in Determination of Velocity Distribution on Airfoils
- On Reflection of Shock Waves from Boundary Layers
- On the Spectrum of Isotropic Turbulence
- Elastic Constants for Corrugated-Core Sandwich Plates
- Effect of Stress-Solvent Crazing on Tensile Strength of Polymethyl Methacrylate
- Skin-Temperature Telemeter for Determining Boundary-Layer Heat-Transfer Coefficients
- Studies on Von Kármán's Similarity Theory and Its Extension to Compressible Flows: A Critical Examination of Similarity Theory for Incompressible Flows
- Resolution of Annealing Experiments for the Study of Nonequilibrium States
- Secondary Flows in Annular Cascades and Effects on Flow in Inlet Guide Vanes
- Effect of Fuel Volatility on Performance of Tail-Pipe Burner
- Supersonic Tunnel Investigation by Means of Inclined-Plate Technique to Determine Performance of Several Nose Inlets Over Mach Number Range of 1.72 to 2.18
- Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flows: A Similarity Theory for Turbulent Boundary Layer Over a Flat Plate in Compressible Flow
- Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flow: Investigation of Turbulent Boundary Layer Over a Flat Plate in Compressible Flow by the Similarity Theory
- Survey of Available Information on Internal Flow Losses Through Axial Turbomachines
- Secondary Stresses in Thin-Walled Beams With Closed Cross Sections
- Methods for Connection to Revolving Thermocouples
- Performance of a Cascade in an Annular Vortex-Generating Tunnel Over Range of Reynolds Numbers
- Application of Variational Methods to Transonic Flows With Shock Waves
- Investigations of Slot Configurations for Film-Cooled Turbine Blades by Flow Visualization Methods
- Deflections of a Simply Supported Rectangular Sandwich Plate Subjected to Transverse Loads
- Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature
- Investigation of the Structural Damping of a Full-Scale Airplane Wing
- Effects of Wing Position and Horizontal-Tail Position on the Static Stability Characteristics of Models With Unswept and 45 Degree Sweptback Surfaces With Some Reference to Mutual Interference
- Effect of Angle of Attack and Exit Nozzle Design on the Performance of a 16-Inch Ram Jet at Mach Numbers From 1.5 to 2.0
- Hydrodynamic Investigation of a Series of Hull Models Suitable for Small Flying Boats and Amphibians
- Generalized Linearized Conical Flow
- Flight Investigation of the Effect of Atmospheric Turbulence on the Climb Performance of an Airplane
- A Flight Investigation of the Effect of Center-of-Gravity Location on Gust Loads
- Study of Vortex Shedding as Related to Self-Excited Torsional Oscillations of an Airfoil
- Theoretical and Experimental Investigation of Additive Drag
- Some Effects of Blade Trailing-Edge Thickness on Performance of a Single-Stage Axial-Flow Compressor
- Review of Problems of Conservation of Strategic Materials for Turbine Engines
- Observations on Bauschinger Effect in Copper and Brass
- Tensile Fracturing Characteristics of Several High-Temperature Alloys as Influenced by Orientation in Respect to Forging Direction
- On the Attached Curved Shock in Front of a Sharp-Nosed Axially Symmetrical Body Placed in a Uniform Stream
- Review of Current and Anticipated Lubricant Problems in Turbojet Engines
- An Electromagnetic Flowmeter for Rocket Research
- Internal Flow and Burning Characteristics of 16-inch Ram Jet Operating in a Free Jet at Mach Numbers of 1.35 and 1.73
- Notes on Heat-Resistant Materials in Britain from Technical Mission October 13 to November 30, 1950
- A Semiempirical Procedure for Computing the Water-Pressure Distribution on Flat and V-Bottom Prismatic Surfaces During Impact or Planing
- Measurements in Flight of the Longitudinal Characteristics of Two Jet Aircraft, One With a Diving Tendency and the Other With a Climbing Tendency at High Mach Numbers
- Influence of Wing and Fuselage on the Vertical-Tail Contribution to the Low-Speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
- Experimental Investigation of the Low-Speed Static and Yawing Stability Characteristics of a 45 Degrees Sweptback High-Wing Configuration with Various Twin Vertical Wing Fins
- Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0