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- Analysis of Sweptback Wings on Cal-Tech Analog Computer
- An Experimental Investigation of the Effect of Wheel Prerotation on Landing-Gear Drag Loads
- Experimental Investigation of Stage Performance of J71 Three-Stage Turbine
- Experimental Determination of Local and Mean Coefficients of Heat Transfer for Turbulent Flow in Pipes
- Heat Transfer, Diffusion, and Evaporation
- Heat Transfer by Free Convection From Horizontal Cylinders in Diatomic Gases
- A Summary of Preliminary Investigations Into the Characteristics of Combustion Screech in Ducted Burners
- Contribution to the Theory of Tail-Wheel Shimmy
- Development of Turbulence-Measuring Equipment
- Kinetic Treatment of the Nucleation in Supersaturated Vapors
- The Plane Problem of the Flapping Wing
- On the Determination of Certain Basic Types of Supersonic Flow Fields
- Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds
- An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds
- A Study of Hypersonic Small-Disturbance Theory
- Investigation of the Effects of Leading-Edge Chord-Extensions and Fences in Combination with Leading-Edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
- Determination of the Elastic Constants of Airplane Tires
- Slowing-Down Distribution to Indium Resonance of Neutrons From a Ra-Alpha-Be Source in Water-Iron Mixtures
- Theoretical Maximum Performance of Liquid Fluorine - Liquid Oxygen Mixtures With JP-4 Fuel as Rocket Propellants
- Pumping Characteristics for Several Simulated Variable-Geometry Ejectors With Hot and Cold Primary Flow
- On the Use of the Indicial-Function Concept in the Analysis of Unsteady Motions of Wings and Wing-Tail Combinations
- Flame Quenching by a Variable-Width Rectangular-Slot Burner as a Function of Pressure for Various Propane-Oxygen-Nitrogen Mixtures
- Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Pitch and Sideslip of Some Canard-Type Missiles Having Cruciform Wings and Canard Surfaces With 70 Degree Delta Plan Forms
- Study of Some Dielectric Properties of Suspensions of Magnesium Particles in Mineral Oil
- A Survey of Background and Aircraft Noise in Communities Near Airports
- Low-Speed Measurements of Rolling and Yawing Stability Derivatives of a 60 Degree Delta-Wing Model
- The Effects of Horizontal-Tail Height and a Partial-Span Leading-Edge Extension on the Static Longitudinal Stability of a Wing-Fuselage-Tail Combination Having a Sweptback Wing
- The Effects of Circular End Plates on the Lift, Drag, and Pitching Moment at Subsonic and Supersonic Speeds on a Modified Triangular Wing Having an Aspect Ratio of 2, a Taper Ratio of 0.33, and a 45 Degree Swept Leading Edge
- Effects of Some Metal Additions on Properties of Molybdenum Disilicide
- An Experimental Investigation of Two-Dimensional, Supersonic Cascade-Type Inlets at a Mach Number of 3.11
- Experimental Evidence of Sustained Coupled Longitudinal and Lateral Oscillations From a Rocket-Propelled Model of a 35 Degree Swept Wing Airplane Configuration
- High-Temperature Lubricants and Bearings for Aircraft Turbine Engine
- Rapid Estimation of Bending Frequencies of Rotating Beams
- Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique
- Preliminary Investigation of Stress-Rupture and Tensile Strength of Thermenol, an Iron-Aluminum Alloy
- Preliminary Measurements of Turbulence and Temperature Fluctuations Behind a Heated Grid
- Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle
- Compatibility of Pentaborane With Materials Used for Seals, Gaskets, and Construction
- Review of High-Performance Axial-Flow-Compressor Blade-Element Theory
- An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds
- Comparison Between Theoretical and Experimental Rates of Roll of Two Models with Flexible Rectangular Wings at Supersonic Speeds
- Investigation of Conical Subsonic Diffusers for Ram-Jet Engines
- Experimental Investigation at High Subsonic Speeds to Determine the Rolling-Stability Derivatives of Three Wing-Fuselage Configurations
- Pressure, Recovery and Mass-Flow Performance of Four Annular Nose Inlets Operating in Mach Number Region of 3.1 and Reynolds Number Range of Approximately 0.45 x 10(exp 6) to 2.20 x 10(exp 6)
- The Effect of a Change in Body Shape on the Loading of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds
- Static Longitudinal Stability Characteristics of a Composite-Plan-Form-Wing-Model Including Some Comparisons with a 45 Degree Sweptback Wing at Transonic Speeds
- Lateral Motions Encountered with the Douglas D-558-II All-Rocket Research Airplane During Exploratory Flights to a Mach Number of 2.0
- Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment
- Application of Pulse Techniques to Strain Gages
- Investigation of Turbojet Engine Performance at Speeds and Gas Temperatures Above Rated Using Turbine-Blade External Water-Spray Cooling from Stationary Injection Orifices