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- Wind-Tunnel Tests on Various Types of Dive Brakes Mounted in Proximity of the Leading Edge of the Wing
- Test Report on Three- and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Trapezoidal Wing)
- Flow Pattern in a Converging-Diverging Nozzle
- Lame's Wave Functions of the Ellipsoid of Revolution
- Flight Investigation of 6.25-Inch-Diameter Deacon Rocket and 10-Inch-Scale Model Rocket
- Some New Problems on Shells and Thin Structures
- Spin and Recovery Characteristics of the Northrop XF-89 Airplane
- The Static-Pressure Error of a Wing Airspeed Installation of the McDonnell XF-88 Airplane in Dives to Transonic Speeds
- Investigation in Simulated Vertical Descent of the Characteristics of a Cargo-Dropping Device having Extensible Rotating Blades
- Investigation of a Systematic Group of NACA 1-Series Cowlings With and Without Spinners
- Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems
- Aerodynamic Characteristics of a 0.5-Scale Model of the Fairchild XSAM-N-2 Lark Missile at High Subsonic Speeds
- Response of a Rotating Propeller to Aerodynamic Excitation
- Experimental study of flow past turbine blades
- Critical Stress of Ring-Stiffened Cylinders in Torsion
- Vibration Survey of Blades in 10-Stage Axial-Flow Compressor 1: Static Investigation
- Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes With Tab Control: Second Partial Report: Application of the Solutions Obtained in the First Partial Report to Tab-Controlled Airplanes
- Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3
- High-Speed Wind-Tunnel Investigation of a Sweptback Wing With an Added Triangular Area at the Center
- General Theory of Aerodynamic Instability and the Mechanism of Flutter
- Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)
- Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
- Aerodynamic Properties of Cruciform-Wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
- A Statistical Study of Wave Conditions at Four Open-Sea Localities in the North Pacific Ocean
- Ambient Pressure Determination at High Altitudes by Use of Free-Molecule Theory
- Wind-tunnel investigation of the spinning characteristics of a model of a twin-tail low-wing personal-owner-type airplane with linked and unlinked rudder and aileron controls