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- Thermodynamic Properties of Gaseous Nitrogen
- Time Correlator for Problems in Aerodynamics
- Effect of Carriage Mass Upon the Loads and Motions of a Prismatic Body During Hydrodynamic Impact
- Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds
- Mechanism of Generation of Pressure Waves at Flame Fronts
- Investigation of Far Noise Field of Jets 1: Effect of Nozzle Shape
- Vapor-Phase Oxidation and Spontaneous Ignition-Correlation and Effect of Variables
- Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy
- Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds
- Charts for Estimating Rotor-Blade Flapping Motion of High-Performance Helicopters
- A Simplified Method for Approximating the Transient Motion in Angles of Attack and Sideslip During a Constant Rolling Maneuver
- Measurement of Static Pressure on Aircraft
- Remark on the Theory of Lifting Surfaces
- On the Gas Dynamics of a Rotating Impeller
- A Flat Wing With Sharp Edges in a Supersonic Stream
- Formation of a Vortex at the Edge of a Plate
- Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack -- Subsonic, Transonic, and Supersonic Speeds
- On the Buckling of Bars and Plates in the Plastic Range: Part 2
- Second-Order Subsonic Airfoil Theory Including Edge Effects
- Torsional Stiffness of Thin-Walled Shells Having Reinforcing Cores and Rectangular, Triangular, or Diamond Cross Section
- The Similarity Rules for Second-Order Subsonic and Supersonic Flow
- Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy
- Theoretical Calculations of the Pressure, Forces, and Moments at Supersonic Speeds Due to Various Lateral Motions Acting on Thin Isolated Vertical Tails
- Interim Report on Fatigue Characteristics of a Typical Metal Wing
- Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8
- Dynamic Investigation of Release Characteristics of a Streamlined Internal Store From a Simulated Bomb Bay of the Republic F-105 Airplane at Mach Numbers of 0.8, 1.4, and 1.98, Coord. No. AF-222
- Directional Stability of Towed Airplanes
- Some Observations on the Relationship Between Fatigue and Internal Friction
- Simplified Method for Estimating Compressible Laminar Heat Transfer With Pressure Gradient
- A Survey and Evaluation of Flutter Research and Engineering
- Theoretical Loss Relations for Low-Speed Two-Dimensional-Cascade Flow
- Torsional Instability of Hinged Flanges Stiffened by Lips and Bulbs
- Torsional Stiffness of Thin-Walled Shells Having Reinforcing Cores and Rectangular, Triangular, or Diamond Cross Section
- Interaction of Bearing and Tensile Loads on Creep Properties of Joints
- A Self-Balancing Line-Reversal Pyrometer
- Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 of Various Tip Controls on the Wing Panel of a 0.05-Scale Model of a Martin XASM-N-7 (Bullpup) Missile: TED No. NACA AD 3106
- Band-Pass Shock and Vibration Absorbers for Application to Aircraft Landing Gear
- Static-Thrust Measurements of the Aerodynamic Loading on a Helicopter Rotor Blade
- A Study by Means of a Dynamic-Model Investigation of the Use of Canard Surfaces as an Aid in Recovering From Spins and as a Means for Preventing Directional Divergence Near the Stall
- Selection of Optimum Configurations for Heat Exchanger With One Dominating Film Resistance
- Application of Scattering Theory to the Measurement of Turbulent Density Fluctuations by an Optical Method
- Light Diffusion Through High-Speed Turbulent Boundary Layers
- Low-Speed Wake Characteristics of Two-Dimensional Cascade and Isolated Airfoil Sections
- Limited Investigation of Effects of Differential Horizontal-Tail Deflection on Lateral Control Characteristics of Two Swept-Wing Airplane Models at Mach Numbers From 1.4 to 2.0
- Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications
- Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane
- Model Ditching Investigation of a Jet Transport Airplane With Various Engine Installations
- Experimental Hinge Moments on Freely Oscillating Flap-Type Control Surfaces
- Investigation of the Ni(sub 3)Al Phrase of Nickel-Aluminum Alloys
- Experimental Investigation at Low Speed of the Effects of Wing Position on the Static Stability of Models Having Fuselages of Various Cross Section and Unswept and 45 Degrees Sweptback Surfaces