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- Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9
- Comparison of Calculated and Measured Thermal Distortions in a Reactor Control Rod for Temperature Patterns Simulating Two Reactor Operating Conditions
- Performance of a Normal-Shock Scoop Inlet with Boundary-Layer Control
- The Synthesis of Butylsilanes by a Large-Scale Reduction with Lithium Aluminum Hydride
- Control Hinge-Moment and Effectiveness Characteristics of a Horn-Balanced, Flap-Type Control on a 55 Degree Sweptback Triangular Wing of Aspect Ratio 3.5 at Mach Numbers of 1.41, 1.62, and 1.96
- Tests of the NACA 0010-1.50 40/1.051 Airfoil Section at High Subsonic Mach Numbers
- The Sodium Hydroxide Reactor - Effect of Reactor Variables on Criticality and Fuel- Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion
- Preliminary Results of Heat Transfer from a Stationary and Rotating Ellipsoidal Spinner
- Stability and Control Characteristics at High Subsonic Speeds of a 1/30-Scale Model of the MX-1554A Design
- Stability and Control Characteristics at Low Speed of a Modified 1/10-Scale Model of the MX-1554A Design
- Stability and Control Characteristics at Low Speed of a 1/10-Scale Model of MX-1554A Design
- An Investigation of the Dynamic and Static Stability Characteristics of a Group of Specialized Store Configurations at Transonic Speeds
- Transonic Aerodynamic and Trim Characteristics of 1/15-Scale Models of the Convair MX-1964 Airplane With Indented Fuselage
- Results of a Power-on Flight of a 1/10-Scale Rocket-Propelled Model of the Convair XF2Y-1 Airplane at a Mach Number of 1.53
- Theoretical Performance of Liquid Hydrogen and Liquid Fluorine as a Rocket Propellant
- Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85
- Wind-Tunnel Investigation of the Drag and Lateral-Stability Characteristics of a 1/22-Scale Model of a Bomber Airplane Employing a Low-Aspect-Ratio Triangular Wing
- Theoretical Performance of Mixtures of Liquid Ammonia and Hydrazine as Fuel With Liquid Fluorine as Oxidant for Rocket Engines
- Theoretical Performance of Liquid Hydrazine and Liquid Fluorine as a Rocket Propellant
- Theoretical Performance of Liquid Ammonia and Liquid Fluorine as a Rocket Propellant
- An Investigation Utilizing an Electrical Analogue of Cyclic Deicing of Hollow Steel Propellers with Internal Electric Heaters
- Impingement of Water Droplets on NACA 65(1)-208 and 65(1)-212 Airfoils at 4 Degrees Angle of Attack
- Maximum Evaporation Rates of Water Droplets Approaching Obstacles in the Atmosphere Under Icing Conditions
- The Effects of Extensible Rocket Racks on Lift, Drag, and Stability of a 1/10 Scale Rocket-Boosted Model of the McDonnell XF3H-1 Airplane for a Mach Number Range of 0.60 to 1.34
- Development of a Supersonic Area Rule and an Application to the Design of a Wing-Body Combination Having High Lift-to-Drag Ratios
- Drag and Static Stability at Low Lift of Rocket-Powered Models of the Convair MX-1626 Airplane at Mach Numbers From 0.7 to 1.5
- Effect of Ice and Frost Formations on Drag of NACA 65(sub 1) -212 Airfoil for Various Modes of Thermal Ice Protection
- Nonuniform Burnup and Poisoning Effects in a Reactor and Validity of Uniform Approximation
- Rocket Engine Starting With Mixed Oxides of Nitrogen and Liquid Ammonia by Flow-Line Additives
- Effect of Fuel Injectors and Liner Design on Performance of an Annular Turbojet Combustor With Vapor Fuel
- Examination of Recent Lateral-Stability-Derivative Data
- An Analysis of a Nuclear Powered Supercritical-Water Cycle for Aircraft Propulsion
- Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free-Jet Facility at Mach Number 3.0
- Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow
- A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds
- A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions
- Investigation of Aerodynamic and Icing Characteristics of a Flush Alternate Inlet Induction System Air Scoop
- Analytical Studies of the Response to Longitudinal Control of Three Airplane Configurations in Landing Approaches
- Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers
- Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conductive to Low Transonic Drag Rise
- Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-Aspect-Ratio Swept-Back Wing-Stability and Control
- Icing Protection for a Turbojet Transport Airplane: Heating Requirements, Methods of Protection, and Performance Penalties
- Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water With Variable Fluid Properties in a Smooth Tube
- Measurement and Analysis of Turbulent Flow Containing Periodic Flow Fluctuations
- The Effect of Blade-Section Camber on the Stall-Flutter Characteristics of Three NACA Propellers at Zero Advance
- Physical Properties of Concentrated Nitric Acid
- The Planing Characteristics of Two v-Shaped Prismatic Surfaces Having Angles of Dead Rise of 20 Degrees and 40 Degrees
- On the Development of Turbulent Wakes from Vortex Streets
- A Preliminary Study of the Problem of Designing High-Speed Airplanes With Satisfactory Inherent Damping of the Dutch Roll Oscillation
- A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer