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- A Preliminary Investigation of High-Speed Impact the Penetration of Small Spheres Into Thick Copper Targets
- Triangular and Intergranular Fracture of Ingot Iron During Creep
- The Theory of Diffusion in Strained Systems
- Theoretical Distribution of Laminar-Boundary-Layer Thickness, Boundary-Layer Reynolds Number and Stability Limit, and Roughness Reynolds Number for a Sphere and Disk in Incompressible Flow
- Influence of Solid-Body Rotation on Screen-Produced Turbulence
- An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
- Some Effects of Vanes and of Turbulence in Two-Dimensional Wide-Angle Subsonic Diffusers
- Lag in Pressure Systems at Extremely Low Pressures
- Method for Determining the Need to Rework or Replace Compressor Rotor Blades Damaged by Foreign Objects
- An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations
- Use of Short Flat Vanes for Producing Efficient Wide-Angle Two-Dimensional Subsonic Diffusers
- Effect of Dissociation on Exhaust-Nozzle Performance
- Discrete Potential Theory for Two-Dimensional Laplace and Poisson Difference Equations
- Approximate Method for Calculation of Laminar Boundary Layer With Heat Transfer on a Cone at Large Angle of Attack in Supersonic Flow
- Free-Flight Investigation to Determine the Drag of Flat- and Vee- Windshield Canopies on a Parabolic Fuselage With and Without Transonic Indentation Between Mach Numbers of 0.75 and 1.35
- Charts Relating the Compressive and Shear Buckling Stresses of Longitudinally Supported Plates to the Effective Deflectional Stiffness
- Performance of a Two-Dimensional Cascade Inlet at a Free-Stream Mach Number of 3.05 and at Angles of Attack of -3 Degrees, 0 Degrees, 3 Degrees, and 6 Degrees
- Effects of Canard Surface Size on Stability and Control Characteristics of Two Canard Airplane Configuration at Mach Numbers of 1.41 and 2.01
- Handbook of Structural Stability Part 6: Strength of Stiffened Curved Plates and Shells
- High-Speed Hydrodynamic Characteristics of a Flat Plate and 20 Degrees Dead-Rise Surface in Unsymmetrical Planing Conditions
- Mass Transfer Cooling Near the Stagnation Point
- On Pairs of Solutions of a Class of Internal Viscous Flow Problems With Body Forces
- Ground Simulator Studies of a Small Side-Located Controller in a Power Control System
- Turbojet Engine Noise Reduction With Mixing Nozzle-Ejector Combinations
- Experimental Investigation of the Effect of Circumferential Inlet Flow Distortion on the Performance of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages
- Static Longitudinal and Lateral Stability Characteristics at Low Speed of 60 Degree Sweptback-Midwing Models Having Wings with an Aspect Ratio of 2, 4, or 6
- Effect of Some External Crosswise Stiffeners on the Heat Transfer and Pressure Distribution on a Flat Plate at Mach Numbers of 0.77, 1.39, and 1.98
- Compressive Strength and Creep of 17-7 PH Stainless-Steel Plates at Elevated Temperatures
- Second-Order Slender-Body Theory: Axisymmetric Flow
- Experimental Lift-Drag Ratios for Two Families of Wing-Body Combinations at Supersonic Speeds
- Transient Heating Effects on the Bending Strength of Integral Aluminum-Alloy Box Beams
- Effect of Temperature on Dynamic Modulus of Elasticity of Some Structural Alloys
- Measurements in a Shock Tube of Heat-Transfer Rates at the Stagnation Point of a 1.0-Inch-Diameter Sphere for Real-Gas Temperatures Up to 7,900 R
- An Approximate Method for Design or Analysis of Two-Dimensional Subsonic-Flow Passages
- Flight Investigation of a Full-Scale Aircraft Ejector with Various Spacing Ratios and Correlation with Small-Scale Tests
- Simulator Investigation of Command Reaction Controls
- The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
- A Simulator Investigation of Factors Affecting the Design and Utilization of a Stick Pusher for the Prevention of Airplane Pitch-Up
- Lift and Moment on Thin Arrowhead Wings with Supersonic Edges Oscillating in Symmetric Flapping and Roll and Application to the Flutter of an All-Moveable Control Surface
- Tables and Graphs of Normal-Shock Parameters at Hypersonic Mach Numbers and Selected Altitudes
- Effect of Advance Ratio on Flight Performance of a Modified Supersonic Propeller
- On Fully Developed Channel Flows: Some Solutions and Limitations, and Effects of Compressibility, Variable Properties, and Body Forces
- Experimental Investigation of Distortion Removal Characteristics of Several Free-Wheeling Fans
- Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
- Some Static Longitudinal Stability Characteristics of an Overlapped-Type Tandem-Rotor Helicopter at Low Airspeeds
- Reflection and Transmission of Sound by a Slotted Wall Separating Two Moving Fluid Streams
- Investigation of the Performance and Internal Flow of a Variable-Area, Variable-Internal-Contraction Inlet at Mach Numbers of 2.00, 2.50, and 2.92
- Transonic Wind-Tunnel Investigation of the Effect of Horizontal Tail on Longitudinal Stability of Two 60 Degree Sweptback-Wing-Body Configurations with Aspect Ratios of 2.67 and 4.00
- Temperature-Pressure-Time Relations in a Closed Cryogenic Container
- Flight Measurements of the Vibratory Stresses on a Propeller Designed for an Advance Ratio of 4.0 and a Mach Number of 0.82