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Effect of Taper Ratio on Lift, Drag, and Pitching-Moment Characteristics of Thin Wings of Aspect Ratio 3 With 53.1 Degrees Sweepback of Leading Edge at Subsonic and Supersonic Speeds

A Simplified Method for Calculating Aeroelastic Effects on the Roll of Aircraft

Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes

Comparison of the Static Stability of a 68.7 Degree Delta-Wing Model with Dihedral and a Twisted and Cambered Wing Model of the Same Plan Form

Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing

Effect of Dissolved Oxygen on the Filterability of Jet Fuels for Temperatures Between 300 Degrees and 400 Degrees Fahrenheit

Note on Hovering Turns with Tandem Helicopters

Effects of Wing-Mounted Tank-Type Stores on the Low Lift Buffeting and Drag of a Swept-Wing Airplane Configuration Between Mach Numbers of 0.8 and 1.3

Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane

Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

Experimental Investigation of a 0.4 Hub-Tip Diameter Ratio Axial-Flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers 2: Stage and Blade-Element Performance

Investigation of Two Short Annular Diffuser Configurations Utilizing Section and Injection as a Means of Boundary-Layer Control

A Theoretical Investigation of a Compensating Network With Application to Roll Control Systems for Automatic Interceptors

Experimental Investigation at High Subsonic Speeds of the Rolling Stability Derivatives of a Complete Model with an Aspect-Ratio-2.52 Wing Having an Unswept 72-Percent-Chord Line and a High Horizontal tail

Performance of Pure Fuels in Single J33 Combustors 2: Hydrocarbon and Nonhydrocarbon Fuels

A Method for Studying the Transient Blade-Flapping Behavior of Lifting Rotors at Extreme Operating Conditions

Results of Measurements Made During the Approach and Landing of Seven High-Speed Research Airplanes

A Correlation of Airfoil Section Data with the Aerodynamic Loads Measured on a 45 Degree Sweptback Wing Model at Subsonic Mach Numbers

Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines

Component Operating Trends During Acceleration and Deceleration of Two Hypothetical Two-Spool Turbojet Engines

Effect of Temperature on Viscosity of Slurries of Boron and Magnesium in JP-5 Fuel

Performance and Component Frontal Areas of a Hypothetical Two-Spool Turbojet Engine for Three Modes of Operation

Some Dielectric Properties of Suspensions of Boron Powders in Mineral Oil

Performance of a Tubular Turbojet Combustor at High Pressures and Temperatures

Comparative Dispersion Data From Ground-Launched 2.25-Inch Rockets Equipped With Cruciform and Monoplane Fins

Steady Properly-Banked Turns of Turbojet-Propelled Airplanes

A Method of Quadrature for Calculation of the Laminar and Turbulent Boundary Layer in Case of Plane and Rotationally Symmetrical Flow

General Solutions of Optimum Problems in Nonstationary Flight

Incompressible Flutter Characteristics of Representative Aircraft Wings

Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure

Theory of Dynamic Creep

Theory of Reversible and Nonreversible Cracks in Solids

Influence of Alloying upon Grain-Boundary Creep

Metallography of Aluminum and Its Alloys: Use of Electrolytic Polishing

Influence of Hot-Working Conditions on High-Temperature Properties of a Heat-Resistant Alloy

Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds

Contributions on the Mechanics of Boundary-Layer Transition

Charts for Estimating Performance of High-Performance Helicopters

Characteristics of Turbulence in Boundary Layer with Zero Pressure Gradient

Some Results of Flight Testing of Ski-Equipped Aircraft at the Naval Air Test Center

Investigation of a Cermet Gas-Turbine-Blade Material of Titanium Carbide Infiltrated With Hastalloy C

Study of Effects of Microstructure and Anisotropy on Fatigue of 23S-T4 Aluminum Alloy

Application of Stream-Filament Techniques to Design of Diffuser Between Compressor and Combustor in a Gas-Turbine Engine

Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

The Effect of a 4-Percent-High Spoiler on Buffeting Forces on a NACA 65(Sub 06)A004 Two-Dimensional Airfoil at Subsonic Mach Numbers

Effects of Wing Position and Fuselage Size on the Low-Speed Static Rolling Stability Characteristics of a Delta-Wing Model

Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips

Free-Flight Tests to Determine the Power-on and Power-Off Pressure Distribution and Drag of the NACA RM-10 Research Vehicle at Large Reynolds Numbers Between Mach Numbers 0.8 and 3.0

A Heated-Wire Liquid-Water-Content Instrument and Results of Initial Flight Tests in Icing Conditions

Quasi-Cylindrical Theory of Wing-Body Interfernece at Supersonic Speeds and Comparison With Experiment


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