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- 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
- Wind-Tunnel Investigation of the Low-Speed Static Longitudinal Characteristics of the Republic RF-84F Airplane
- Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro-Skis: TED No. NACA DE 357
- Time Variation of the Distance Separating Bomb and Dive Bomber Subsequent to Bomb Release
- Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman F9F-6 Airplane: TED No. NACA DE 364
- Thrust Augmentation of a Turbojet Engine at Simulated Flight Conditions by Introduction of a Water-Alcohol Mixture into the Compressor
- Hydrocarbon and nonhydrocarbon derivatives of cyclopropane
- The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements
- Dynamic response at altitude of a turbojet engine with variable area exhaust nozzle
- Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane
- Theoretical and experimental investigation of mufflers with comments on engine-exhaust muffler design
- Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
- Effect of initial mixture temperature on flame speed of methane-air, propane-air, and ethylene-air mixtures
- Two-and three-dimensional unsteady lift problems in high-speed flight
- Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane
- Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane