Effect of Reflex Camber on the Aerodynamic Characteristics of a Highly Tapered Moderately Swept-back Wing at Reynolds Numbers up to 8,000,000
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Conner, D William↗
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Results for “moderator”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Effects of Moderate Biaxial Stretch-forming on Tensile and Crazing Properties of Acrylic Plastic Glazing
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Axilrod, B M↗
Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio
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Deyoung, John↗
The effect of Reynolds number on the stalling characteristics and pressure distributions of four moderately thin airfoil sections
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Mccullough, George B↗
Flight Investigation of Effects of Atmospheric Turbulence and Moderate Maneuvers on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
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Ludi, Leroy H↗
An empirically derived method for calculating pressure distribution at supercritical Mach numbers and moderate angles of attack
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Nitzberg, Gerald E↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics for Symmetrical Wing Sections at High Subsonic and Moderate Supersonic Mach Numbers
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Mas, Newton A↗
Some Effects of Chordwise Fences on the Aerodynamic Characteristics of Four Moderately Sweptback Wings in the Low-lift Range at Transonic Mach Numbers and at Mach Number 1.9
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Guy, Lawrence D↗
An experimental study at moderate and high subsonic speeds of the flow over wings with 30 degrees and 45 degrees of sweepback in conjunction with a fuselage
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Whitcomb, Richard T↗
An experimental study at moderate and high subsonic speeds of the flow over wings with 30 degrees and 45 degrees of sweepforward in conjunction with a fuselage
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Whitcomb, Richard T↗
An experimental study at moderate and high subsonic speeds of the flow over an unswept wing in conjunction with a fuselage
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Whitcomb, Richard T↗
Force tests of three thin wings of moderately low aspect ratio at high subsonic Mach numbers
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Jordan, Gareth H↗
Calculated effect of uranium distribution on reflector control effectiveness for a water-moderated power reactor
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Fox, Thomas A↗
Altitude-wind-tunnel Investigation of Several Afterburner Configurations Having Moderately High Burner-inlet Velocities
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Schulze, F W↗
A method for designing low-drag nose-inlet--body combinations for operation at moderate supersonic speeds
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Howell, Robert R↗
Experimental Investigation of Some Aerodynamic Effects of a Gap Between Wing and Body of a Moderately Slender Wing-body Combination at a Mach Number of 1.4
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Dugan, Duane W↗
Experimental study of a method of designing the sweptback-wing-fuselage juncture to reduce the drag at moderate supersonic speeds
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Howell, Robert R↗
Effect of Moderate Air Flow on the Distribution of Fuel Sprays After Injection Cut-0ff
High-speed motion pictures were taken of fuel sprays with the NACA spray-photographic apparatus to study the distribution of the liquid fuel from the instant of injection cut-off until about 0.05 second later. The fuel was injected into a glass-walled chamber in which the air density was varied from 1 to 13 times atmospheric air density (0.0765 to 0.99 pound per cubic foot) and in which the air was at room temperature. The air in the chamber was set in motion by means of a fan, and was directed counter to the spray at velocities up to 27 feet per second. The injection pressure was varied from 2,000 to 6,000 pounds per square inch. A 0.20-inch single-orifice nozzle, an 0.008-inch single-orifice nozzle, a multiorifice nozzle, and an impinging-jets nozzle were used. The best distribution was obtained by the use of air and a high-dispersion nozzle.
Rothrock, A M↗