Effects Of Twist And Camber On The Low Speed Longitudinal Stability Characteristics Of A 45 O Sweptback Wing Of Aspect Ratio 8 At Reynolds Numbers From 15 X 10 6 To 48 X 10 6 As Determined By Pressure Distributions Force Tests And Calculations PDF Download
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Author | : George L. Pratt |
Publisher | : |
Total Pages | : 110 |
Release | : 1952 |
Genre | : Airplanes |
ISBN | : |
Download Effects 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 Book in PDF, ePub and Kindle
Author | : George L. Pratt |
Publisher | : |
Total Pages | : 104 |
Release | : 1952 |
Genre | : |
ISBN | : |
Download 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 Book in PDF, ePub and Kindle
Author | : George L. Pratt |
Publisher | : |
Total Pages | : |
Release | : 1952 |
Genre | : |
ISBN | : |
Download Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 O 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 Book in PDF, ePub and Kindle
Author | : George L. Pratt |
Publisher | : |
Total Pages | : |
Release | : 1952 |
Genre | : |
ISBN | : |
Download 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 Book in PDF, ePub and Kindle
Author | : Gerald V. Foster |
Publisher | : |
Total Pages | : 30 |
Release | : 1952 |
Genre | : |
ISBN | : |
Download Effects of Twist and Camber, Fences and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristcs of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 X (10)6 Book in PDF, ePub and Kindle
Author | : Lynn W. Hunton |
Publisher | : |
Total Pages | : 36 |
Release | : 1950 |
Genre | : |
ISBN | : |
Download Effects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1952 |
Genre | : |
ISBN | : |
Download Effect of Linear Spanwise Variations of Twist and Circular-Arc Camber on Low-Speed Static Stability, Rolling, and Yawing Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 4 and Taper Ration 0.6 Book in PDF, ePub and Kindle
An investigation at low scale has been made in the Langley stab unity tunnel in order to determine the effect of linear spanwise variations of twist and circular-arc camber on the low-speed aerodynamic characteristics and static-stability and rotary-stability (rolling and yawing) derivatives of a wing of aspect ratio 4, taper ratio 0.6, and with 45 deg sweepback of the quarter-chord line. Results of the investigation indicate that twist or camber produced only small changes in the maximum lift coefficient. A combination of camber and twist was more effective than twist alone in providing an increase in the maximum lift-to-drag ratio in the moderate lift-coefficient range for the wings investigated. The variation of static longitudinal stability through the lift-coefficient range was less for the twisted wing than for the twisted and cambered or plane wing. A combination of twist and camber generally extended the initial linear range of several of the static- and rotary-stability derivatives to a higher lift coefficient and, although these effects were small, higher Reynolds numbers may result in larger effects.
Author | : Robert R. Graham |
Publisher | : |
Total Pages | : 54 |
Release | : 1951 |
Genre | : |
ISBN | : |
Download Low-speed Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 8 from Pressure Distributions and Force Tests at Reynolds Numbers from 1,500,000 to 4,800,000 Book in PDF, ePub and Kindle
Author | : Byron M. Jaquet |
Publisher | : |
Total Pages | : 27 |
Release | : 1952 |
Genre | : |
ISBN | : |
Download Effect of Linear Spanwise Variations of Twist and Circular-arc Camber on Low-speed Static Stability, Rolling, and Yawing Characteristics of a 45 [degrees] Sweptback Wing of Aspect Ratio 4 and Taper Ratio 0.6 Book in PDF, ePub and Kindle
Author | : Gerald V. Foster |
Publisher | : |
Total Pages | : 44 |
Release | : 1955 |
Genre | : |
ISBN | : |
Download 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 Book in PDF, ePub and Kindle