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- A study of the transient behavior of shock waves in transonic channels flows
- Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers
- Analytical and experimental investigation of fully developed turbulent flow of air in a smooth tube with heat transfer with variable fluid properties
- Transonic similarity rules for lifting wings
- Use of the boundary layer of a cone to measure supersonic flow inclination
- An analysis of the normal accelerations and airspeeds of a two-engine type of transport airplane in commercial operations on routes in the central United States from 1948 to 1950
- A theory and method for applying interferometry to the measurement of certain two-dimensional gaseous density fields
- Wear and sliding friction properties of nickel alloys suited for cages of high-temperature rolling-contact bearings II : alloys retaining mechanical properties above 600 F
- The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design
- A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock
- Experimental investigation of a 90 degree cascade diffusing bend with an area ratio of 1.45:1 and with several inlet boundary layers
- Orientation of orifices on bodies of revolution for determination of stream static pressure at supersonic speeds
- Comparison of supersonic minimum-drag airfoils determined by linear and nonlinear theory
- Comparison of two- and three-dimensional potential-flow solutions in a rotating impeller passage
- Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6
- Effects of wing sweep on the upwash at the propeller planes of multiengine airplanes
- Effects of wing lift and weight on landing-gear loads
- Effects of solvents in improving boundary lubrication of steel by silicones
- Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control
- On the calculation of flow about objects traveling at high supersonic speeds
- Stress and strain at onset of crazing of polymethyl methacrylate at various temperatures
- Wear and sliding friction properties of nickel alloys suited for cages of high-temperature rolling-contact bearings I : alloys retaining mechanical properties to 600 F
- Condensation of air in supersonic wind tunnels and its effects on flow about models
- Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges
- A vector study of linearized supersonic flow applications to nonplanar problems
- Investigation with an interferometer of the flow around a circular-arc airfoil at mach numbers between 0.6 and 0.9
- Laminar boundary layer on cone in supersonic flow at large angle of attack
- A probability analysis of the meteorological factors conducive to aircraft icing in the United States
- Gust-response analysis of an airplane including wing bending flexibility
- Displacement effect of a three-dimensional boundary layer
- Some experiments on visualization of flow fields behind low-aspect-ratio wings by means of a tuft grid
- Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds
- Experimental investigation of transition of a model helicopter rotor from hovering to vertical autorotation
- Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) power on the maximum lift coefficient of a wing of NACA 64-210 airfoil sections
- A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)
- Summary of stall-warning devices
- flow studies in the vicinity of a modified flat-plate rectangular wing of aspect ratio 0.25
- Measurements of temperature variations in the atmosphere near the tropopause with reference to airspeed calibration by the temperature method
- A compressible-flow plotting device and its application to cascade flows
- Boundary-layer development and skin friction at mach number 3.05
- Altitude Investigation of Gas Temperature Distribution at Turbine of Three Similar Axial-Flow Turbojet Engines
- Summary of Low-Lift Drag and Directional Stability Data from Rocket Models of the Douglas XF4D-1 Airplane with and without External Stores and Rocket Packets at Mach Numbers from 0.8 to 1.38: TED No. NACA DE-349
- Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket
- Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings
- Theoretical Investigation of the Effects of the Artificial-Feel System on the Maneuvering Characteristics of the F-89 Airplane
- Analytical study of shimmy of airplane wheels
- Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
- Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow
- Experimental investigation of free-convection heat transfer in vertical tube at large Grashof numbers
- Internal-liquid-film-cooling experiments with air-stream temperatures to 2000 degrees F. in 2- and 4-inch-diameter horizontal tubes