The Effect of Rate of Change of Angle of Attack on the Maximum Lift Coefficient of a Pursuit Airplane
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Gadeberg, Burnett L↗
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Results for “maximum”
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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Theoretical investigation of velocity diagrams of a single-stage turbine for a turbojet engine at maximum thrust per square foot turbine frontal area
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Cohen, Leo↗
Langley Full-scale-tunnel Investigations of the Maximum-lift and Stalling Characteristics of a Trapezoidal Wing of Aspect Ratio 4 with Circular-arc Airfoil Sections
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Lange, Roy H↗
Effects of Independent Variations of Mach Number and Reynolds Number on the Maximum Lift Coefficients of Four NACA 6-series Airfoil Sections
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Racisz, Stanley F↗
Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers
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Stone, Ralph W , Jr↗
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
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SURFACE CONDITIONS - COMPLETE WINGS↗
Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections
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Berggren, Robert E↗
Effect of variation in rivet strength on the average stress at maximum load for aluminum-alloy, flat, z-stiffened compression panels that fail by local buckling
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Dow, Norris F↗
Maximum theorems and reflections of simple waves
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Germain, P↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Some Observations on Maximum Pressure Rise Across Shocks Without Boundary-layer Separation on Airfoils at Transonic Speeds
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Lindsey, Walter F↗
An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift
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Maki, Ralph L↗
Maximum theoretical tangential velocity component possible from straight-back converging and converging-diverging stators at supercritical pressure ratios
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Moffitt, Thomas P↗
Pressure Distributions at Transonic Speeds for Slender Bodies Having Various Axial Locations of Maximum Diameter
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Mcdevitt, John B↗
Investigation of Minimum Drag and Maximum Lift-drag Ratios of Several Wing-body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and diamond plan form are presented for Mach numbers of 1.62, 1.93, and 2.41 and a Reynolds number range of 1.4 x 10 to the 6th power to 0.7 x 10 to the 6th power. Included are two each of triangular and arrow plan-form wings cambered for approximately uniform load at m = 1.62 and lift coefficients of 0.08 and 0.20. Liquid-film studies of the flow over the various configurations are also presented.
Brown, Clinton E↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area II : Effects of Slots upon an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody
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Goldstein, David L↗
Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter
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Thompson, Jim Rogers↗
Effect of Leading-edge High-lift Devices and Split Flaps on the Maximum-lift and Lateral Characteristics of a Rectangular Wing of Aspect Ratio 3.4 with Circular-arc Airfoil Sections at Reynolds Numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).
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Lange, Roy H↗