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- 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
- Effects of Several Arrangements of Rectangular Vortex Generators on the Static-Pressure Rise Through a Short 2:1 Diffuser
- Effects of Design Details on the Fatigue Strength of 355-T6 Sand-Cast Aluminum Alloy
- Evaluation of High-Angle Attack Aerodynamic-Derivative Data and Stall-Flutter Prediction Techniques
- Experimental Pressure Distributions Over Two Wing-Body Combinations at Mach Number 1.9
- Power Unit for High-Intensity Light Source
- Mechanical and Corrosion Tests of Spot-Welded Aluminum Alloys
- Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-Percent-Thick, Biconvex Section
- Preliminary Investigation of the Control of a Gas-Turbine Engine for a Helicopter
- The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45 Degrees of Sweepback, an Aspect Ratio of 3, and a Taper Ratio of 0.5
- Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield
- Combustion-Chamber Performance Characteristics of a Python Turbine-Propeller Engine Investigated in Altitude Wind Tunnel
- Sideslip in a Viscous Compressible Gas
- Lateral Control by Spoilers at the DVL
- On the Problem of Gas Flow Over an Infinite Cascade Using Chaplygin's Approximation
- On the Theory of Thin and Thin-Walled Rods