64 research outputs found
Combined Effects of Wing Taper Ratio and Low Horizontal-Tail Position on Longitudinal Stability of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds
Get PDFLow-speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 x 10(exp 6)
Get PDFLongitudinal Stability Characteristics of a 42 Degree Sweptback Wing and Tail Combination at a Reynolds Number of 6.8 x 10(exp 6)
Get PDFResults are given of a wind-tunnel investigation at a Reynolds number of 6.8 x 10(exp 6) to determine the static longitudinal stability characteristics of a 42 degree sweptback wing and fuselage combination with a sweptback horizontal tail. Included are the effects of vertical position of fuselage and tail with respect to wing for several combinations of high-lift and staff-control devices. Also included is the effect of a simulated ground
Investigation in the Langley 19-foot Pressure Tunnel of Two Wings of NACA 65-210 and 64-210 Airfoil Sections with Various Type Flaps
Get PDFReport presents the results of an investigation conducted in the Langley 19-foot pressure tunnel to determine the maximum lift and stalling characteristics of two thin wings equipped with several types of flaps. Split, single slotted, and double slotted flaps were tested on one wing which had NACA 65-210 airfoil sections and split and double slotted flaps were tested on the other, which had NACA 64-210 airfoil sections. Both wings were zero sweep, an aspect ratio of 9, and a taper ratio of 0.4
Investigation in the Langley 19-Foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps
Get PDFPositioning 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)
Get PDFLow-speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-arc Airfoil Sections at Reynolds Numbers of Approximately 6.0 x 10(exp 6)
Get PDFLow-speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-wing : Fuselage Combination at a Reynolds Number of 6.0 x 10(exp 6)
Get PDFLow-speed pressure distributions over the drooped-nose flap of a 42 degrees sweptback wing with circular-arc airfoil sections at a Reynolds number of 5.3 x 10(exp 6)
Get PDFEffects of High-lift and Stall-control Devices, Fuselage, and Horizontal Tail on a Wing Swept Back 42 Degrees at the Leading Edge and Having Symmetrical Circular-arc Airfoils Sections at a Reynolds Number of 6.9 x 10(exp 6)
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