Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area III : Inlet Enclosing 37.2 Percent of the Maximum Circumference of the Forebody
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Davis, Wallace F↗
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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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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↗
Aerodynamic Characteristics at Subsonic and Supersonic Mach Numbers of a Thin Triangular Wing of Aspect Ratio 2 I : Maximum Thickness at 20 Percent of the Chord
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Berggren, Robert E↗
Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness
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Eggers, A J , Jr↗
Full-scale Investigation of the Maximum Lift and Flow Characteristics of an Airplane Having Approximately Triangular Plan Form
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Wilson, Herbert A , Jr↗
The Effect of Sample Size on the Determination of Maximum Gust Velocities in Clouds
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Press, Harry↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area I : an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody
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Davis, Wallace F↗
Free-fall Measurements at Transonic Velocities of the Drag of a Wing-body Configuration Consisting of a 45 Degree Swept-back Wing Mounted Forward of the Maximum Diameter on a Body of Fineness Ratio 12
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Mathews, Charles W↗
Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds
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Gallagher, James J↗
Maximum lift and longitudinal stability characteristics at Reynolds numbers up to 7.8 x 10(exp 6) of a 35 degree sweptforward wing equipped with high-lift and stall-control devices, fuselage, and horizontal tail
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Martina, Albert P↗
Survey of two-dimensional data on pitching-moment changes near maximum lift caused by deflection of high-lift devices
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Bidwell, Jerold M↗
Maximum-lift investigation at Mach numbers from 0.05 to 1.20 of a wing with leading edge swept back 42 degrees
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Turner, Thomas R↗
Flight Investigation at High-subsonic, Transonic, and Supersonic Speeds to Determine Zero-lift Drag of Bodies of Revolution Having Fineness Ratio of 6.04 and Varying Positions of Maximum Diameter
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Katz, Ellis R↗
Maximum-lift characteristics of a wing with the leading-edge sweepback decreasing from 45 degrees at the root to 20 degrees at the tip at Reynolds numbers from 2.4 x 10(exp 6) to 6.0 x 10(exp 6)
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Lange, Roy H↗
Experimental investigation of the effectiveness of various suction-slot arrangements as a means for increasing the maximum lift of the NACA 65(sub 3)-018 airfoil section
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Racisz, Stanley, F↗
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↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness of an Elevon as a Longitudinal Control and the Effects of Camber and Twist on the Maximum Lift-drag Ratio at Supersonic Speeds
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Olson, Robert N↗