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- Foaming of Mixtures of Pure Hydrocarbons
- Theoretical Analysis of Oscillations in Hovering of Helicopter Blades With Inclined and Offset Flapping and Lagging Hinge Axes
- Pressure Distribution and Damping in Steady Roll at Supersonic Mach Numbers of Flat Swept-Back Wing with Subsonic Edges
- Effects of an Aging Treatment on Life of Small Cast Vitallium Gas-Turbine Blades
- Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 3: Methods for Determining Power and Efficiency
- Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 1: Methods for Determining Heat-Transfer Characteristics
- Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 2: Methods for Determining Cooling-Air-Flow Characteristics
- Downwash in Vortex Region Behind Rectangular Half-Wing at Mach Number 1.91
- Static Directional Stability of a Tandem-Helicopter Fuselage
- Performance of 4600-Pound-Thrust Centrifugal-Flow-Type Turbojet Engine With Water-Alcohol Injection at Inlet
- Dynamic Investigation of Turbine-Propeller Engine Under Altitude Conditions
- Chordwise and Spanwise Loadings Measured at a Large Triangular Wing Having an Aspect Ratio of 2 and a Thin, Subsonic-Type Airfoil Section
- Investigation at High Subsonic Speeds of Methods of Alleviating the Adverse Interference at the Root of a Swept-Back Wing
- Analysis of Multiengine Transport Airplane Fire Records
- Penetration of Liquid Jets into a High-Velocity Air Stream
- Effects of the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane
- Exploratory Investigation of the Effect of Skewed Plain Nose Flaps on the Low-Speed Characteristics of a Large-Scale Triangular-Wing-Fuselage Model
- Low-Speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface
- Effect of an End Plate on the Aerodynamic Characteristics of a 20.55 Degree Sweptback Wing with an Aspect Ratio of 2.67 and a Taper Ratio of 0.5.: Transonic-Bump Method
- Determination of Minimum Moments of Inertia of Arbitrarily Shaped Areas, Such as Hollow Turbine Blades
- Lateral-Control Investigation at a Reynolds Number of 5,300,000 of a Wing of Aspect Ratio 5.8 Sweptforward 32 Degrees at the Leading Edge
- High-Speed Aerodynamic Characteristics of a Lateral-Control Model 2: Modified NACA 0012-64 Section with a 26.6-Percent-Chord, Plain, Trailing-Edge Aileron; Wing Unswept and Swept Back 45 Degrees
- Calculated Performance of Nuclear Turbojet Powered Airplane at Flight Mach Number of 0.9
- A Design Study of Leading-Edge Inlets for Unswept Wings
- Pressure Coefficients at Mach Numbers from 0.60 to 0.85 for a Semispan Wing with NACA 0012-64 Section, 20-Percent-Chord Plain Aileron, and 0 Degree and 45 Degree Sweepback
- Effect of Retractable Ignition Plug on Plug Fouling by Carbon Deposits
- Investigation at a Mach Number of 1.93 to Determine Lift, Drag, Pitching-Moment, and Average Downwash Characteristics for Several Missile Configurations Having Rectangular Wings and Tails of Various Spans
- Further Investigation of a Gas Turbine with National Bureau of Standards Body 4811C Ceramic Rotor Blades
- Altitude-Chamber Performance of British Roll-Royce Nene II Engine 4: Effect of Operational Variables on Temperature Distribution at Combustion-Chamber Outlets
- A Lift-Cancellation Technique in Linearized Supersonic-Wing Theory
- On the Theory of the Propagation of Detonation in Gaseous Systems
- On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid
- Laws of Flow in Rough Pipes
- Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction
- Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed
- Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed
- Dependence of the Elastic Strain Coefficient of Copper on the Pre-Treatment
- The Development of a Hollow Blade for Exhaust Gas Turbines
- General Solution of Prandtl's Boundary-Layer Equation
- Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line
- Effect of Intense Sound Waves on a Stationary Gas Flame
- Theory of Plane, Symmetrical Intake Diffusers
- Turbulence and Heat Stratification
- The Solution of the Laminar-Boundary-Layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration
- The Stability of the Compression Cover of Box Beams Stiffened by Posts
- Contribution to the Problem of Buckling of Orthotropic Plates, With Special Reference to Plywood
- Some Effects of Nonlinear Variation in the Directional-Stability and Damping-in-Yawing Derivatives on the Lateral Stability of an Airplane
- Analysis of Turbulent Free-Convection Boundary Layer on Flat Plate
- The Diffusion of a Hot Air Jet in Air in Motion Part 2: The Flow Field in the Transition Zone
- Graphical Determination of Wall Temperatures for Heat Transfers Through Walls of Arbitrary Shape