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- Analysis of a liquid-metal turbine-propeller cycle for propulsion of low-speed nuclear- powered aircraft
- Wind-Tunnel Investigation of the Contribution of a Vertical Tail to the Directional Stability of a Fighter-Type Airplane
- A Thermodynamic Study of the Turbine-Propeller Engine
- A Low-Speed Investigation of an Annular Transonic Air Inlet
- Radioautographic Method for Examining Distribution of Particles in a Cyclotron Beam
- Effect of Temperatures From -70 to 600 Degrees Fahrenheit on Strength of Adhesive-Bonded Lap Shear Specimens of Clad 24S-T3 Aluminum Alloy and of Cotton-and Glass-Fabric Plastic Laminates
- Several Combination Probes for Surveying Static and Total Pressure and Flow Direction
- A Technique Applicable to the Aerodynamic Design of Inducer-Type Multistage Axial-Flow Compressors
- Flight Investigation of Transient Wing Response on a Four-Engine Bomber Airplane in Rough Air With Respect to Center-of-Gravity Accelerations
- Corrections for Lift, Drag, and Moment of an Airfoil in a Supersonic Tunnel Having a Given Static Pressure Gradient
- X-Ray Instrumentation for Density Measurements in a Supersonic Flow Field
- Supersonic Wave Drag of Nonlifting Delta Wings With Linearly Varying Thickness Ratio
- Wind-Tunnel Investigation of the Effects of Various Asymmetric Canopy Modifications on the Behavior of Descending Parachutes
- A Theoretical Method of Analyzing the Effects of Yaw-Damper Dynamics on the Stability of an Aircraft Equipped With a Second-Order Yaw Damper
- An Impulse-Momentum Method for Calculating Landing-Gear Contact Conditions in Eccentric Landings
- The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel With and Without Nacelles at Mach Numbers From 0.30 to 0.86
- Estimation of the Maximum Angle of Sideslip for Determination of Vertical-Tail Loads in Rolling Maneuvers
- Experimental Determination of Time Constants and Nusselt Numbers for Bare-Wire Thermocouples in High-Velocity Air Streams and Analytic Approximation of Conduction and Radiation Errors
- The Effect of Blade-Section Camber on the Static Characteristics of Three NACA Propellers
- Interaction of Column and Local Buckling in Compression Members
- Short-Bearing Approximation for Full Journal Bearings
- Correlation of Tensile Strength, Tensile Ductility, and Notch Tensile Strength With the Strength of Rotating Disks of Several Designs in the Range of Low and Intermediate Ductility
- Bending of Thin Plates With Compound Curvature
- Buckling of Low Arches or Curved Beams of Small Curvature
- A Low-Speed Investigation of a Fuselage-Side Air Inlet for Use at Transonic Flight Speeds
- Inviscid Flow About Airfoils at High Supersonic Speeds
- Influence of Lubricant Viscosity on Operating Temperatures of 75-Millimeter-Bore Cylindrical-Roller Bearing at High Speeds
- The Gust and Gust-Load Experience of a Twin-Engine Low-Altitude Transport Airplane in Operation on a Northern Transcontinental Route
- Experiments in External Noise Reduction of a Small Pusher-Type Amphibian Airplane
- Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction
- On the Representation of the Stability Region in Oscillation Problems With the Aid of the Hurwitz Determinants
- Preliminary Air-Flow and Thrust Calibrations of Several Conical Cooling-Air Ejectors with a Primary to Secondary Temperature Ratio of 1.0, 2: Diameter Ratios of 1.06 and 1.40
- The Effect of High Viscosity on the Flow Around a Cylinder and Around a Sphere
- Translational Motion of Bodies Under the Free Surface of a Heavy Fluid of Finite Depth
- Structural Vulnerability of the Boeing B-29 Aircraft Wing to Damage by Warhead Fragments
- A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics
- Wind-Tunnel Investigation of the Low-Speed Static Stability and Control Characteristics of a Model of the Bell MX-776 (RASCAL) in Combined Angle of Attack and Sideslip
- Pressure Recovery, Drag, and Subcritical Stability Characteristics of Conical Supersonic Diffusers With Boundary-Layer Removal
- Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes A-3B Missile at a Mach Number of 5.0
- Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section (Including Large Temperature Differences and Transpiration Cooling)
- A Wind-Tunnel Investigation to Determine the Effect of Various Head Designs on the Aerodynamic Characteristics in Pitch of the Army Ordnance Corps T205 3.5-Inch Heat Rocket
- Investigation of Spinning and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultee XFY-1 Airplane in the Free-Spinning Tunnel, TED No. NACA DE 370
- Preliminary Results Obtained from Flight Test of a 1/7-Scale Rocket-Powered Model of the Grumman XF10F Airplane Configuration in the Swept-Wing Condition, TED No. NACA DE 354
- Effect of Various Blade Modifications on Performance of a 16-Stage High-Pressure-Ratio Axial-Flow Compressor 1 - Effect on Over-All Performance Characteristics of Decreasing Twelfth Through Fifteenth State Stator-Blade Angles 3 Degrees
- Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 2 - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 Degrees
- Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 5 - Effect on Over-All Performance Characteristics of a 20-Percent Reduction in Solidity of the Fourteenth Through Sixteenth Stage Rotors
- Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 3 - Effect on Over-All Performance Characteristics on Increasing Stator-Blade Angles in Inlet Stages
- Effect of Rotor- and Stator-Blade Modifications on Surge Performance of an 11-Stage Axial-Flow Compressor 1 - Original Production Compressor of XJ40-WE-6 Engine
- Detailed Computational Procedure for Design of Cascade Blades With Prescribed Velocity Distributions in Compressible Potential Flows
- Ditching Investigation of a 1/12-Scale Model of the Douglas F3D-2 Airplane, TED No. NACA DE 381