Longitudinal Characteristics of Two 47.7 Degree Sweptback Wings with Aspect Ratios of 5.1 and 6.0 at Reynolds Numbers up to 10 x 10(exp 6)
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Salmi, Reino J↗
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Results for “10-Be”
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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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↗
Low-speed longitudinal characteristics of a circular-arc 52 degree sweptback wing of aspect ratio 2.84 with and without leading-edge and trailing-edge flaps at Reynolds numbers from 1.6 x 10(exp 6) to 9.7 x 10(exp 6)
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Foster, Gerald V↗
Effects of inlet wall contour on the pressure recovery of a 10 degrees 10-inch-inlet-diameter conical diffuser
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Copp, Martin R↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) II : Aerodynamic Load Distributions of Series of Five Bodies Having Conical Noses and Cylindrical Afterbodies
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Jack, John R↗
Low-speed Longitudinal Aerodynamic Characteristics of a Twisted and Cambered Wing of 45 Degree Sweepback and Aspect Ratio 8 with and Without High-lift and Stall-control Devices and a Fuselage at Reynolds Numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6
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Salmi, Reino J↗
Investigation of the effects of variations in the Reynolds number between 0.4 x 10(exp 6) 3.0 x 10(exp 6) on the low-speed aerodynamic characteristics of three low-aspect-ratio symmetrical wings with rectangular plan forms
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Jones, George W , Jr↗
Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45 degree sweptback wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6) as determined by pressure distributions, force tests
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Pratt, George L↗
Wind-tunnel Investigation of Stall Control by Suction Through a Porous Leading Edge on a 37 Degree Sweptback Wing of Aspect Ratio 6 at Reynolds Numbers from 2.50 x 10(exp 6) to 8.10 x 10(exp 6)
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Graham, Robert R↗
Low-speed longitudinal characteristics of an unswept hexagonal wing with and without a fuselage and a horizontal tail located at various positions at Reynolds numbers from 2.8 x 10(exp 6) to 7.6 x 10(exp 6)
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Foster, Gerald V↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) III : Boundary Layer and Force Measurements on a Slender Cone-cylinder Body of Revolution
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Jack, John R↗
Experimental Investigation of the Effects of Support Interference on the Pressure Distribution of a Body of Revolution at a Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 14 x 10(exp 6)
A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented. (author)
Baughman, L Eugene↗
Experimental Investigation of the Zero-lift Drag of a Fin-stabilized Body of Fineness Ratio 10 at Mach Numbers Between 0.6 and 10
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James, Carlton S↗
Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45 degree sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10(exp 6) to 8 x 10(ex
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Braslow, Albert L↗
Effects of Increasing Reynolds Number from 2 x 10(exp 6) to 6 x 10(exp 6) on the Aerodynamic Characteristics at Transonic Speeds of a 45 Degree Swept Wing with 6 Degree Leading-edge Droop
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Schmeer, James W↗
Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C(sub zeta(sub o)) A(sub 10)) 10 compressor-blade sections at low speeds
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Savage, Melvyn↗
Two-dimensional Cascade Tests of NACA 65-(c(sub Zeta)(sub O))a(sub 10))10 Blade Sections at Typical Compressor Hub Conditions for Speeds up to Choking
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Emery, James C↗
Positioning Investigation of Single Slotted Flaps on a 47.7 Degrees Sweptback Wing at Reynolds Numbers of 4.0 x 10(exp 6) and 6.0 x 10(exp 6)
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Spooner, Stanley H↗