Author: Gerald V. FosterPublisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Effects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degrees Sweptback Wings Incorporating Leading-edge Camber as Influenced by Reynolds Numbers Up to 8.00 X 10 6 and Mach Numbers Up to 0.290
Author: Gerald V. FosterEffects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degree Sweptback Wings as Influenced by Reynolds Number Up to 8.20 X (10)6 and Mach Numbers Up to 0.303
Author: Gerald V. FosterEffects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. PrattPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110
Book Description
Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers
Author: William C. SchneiderEffects of Reynolds Number and Leading Edge Shape on the Low-speed Longitudinal Stability of a 6 Percent-thick 45 Degree Sweptback Wing
Author: William C. SchneiderThe Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96
Author: Robert I. SammondsPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 64
Book Description
An investigation has been conducted to determine the effect of conical camber on the drag due to lift and on the static longitudinal, lateral, and directional stability characteristics of an aspect-ratio-3, 45 degree sweptback wing in combination with a streamline body. Tests were made at Mach numbers up to 0.96 at a Reynolds number of 1.5 million and at a Reynolds number up to 8 million at a Mach number of 0.22, both with and without roughness strips near the leading edge of both the upper and lower surfaces of the wing.
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)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. PrattEffects 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
Author: George L. PrattEffects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4
Author: Earl D. KnechtelPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.
Author: George L. Pratt