Effect on the Low-speed Aerodynamic Characteristics of a 49 Degree Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron

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ISBN 13 :
Total Pages : 51 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Effect on the Low-speed Aerodynamic Characteristics of a 49 Degree Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron by : Edward F. Jr Whittle

Download or read book Effect on the Low-speed Aerodynamic Characteristics of a 49 Degree Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron written by Edward F. Jr Whittle and published by . This book was released on 1954 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect on the Low-speed Aerodynamic Characteristics of a 49 Degrees Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Effect on the Low-speed Aerodynamic Characteristics of a 49 Degrees Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron by : Jr. Edward F. Whittle

Download or read book Effect on the Low-speed Aerodynamic Characteristics of a 49 Degrees Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron written by Jr. Edward F. Whittle and published by . This book was released on 1954 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (78 download)

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Book Synopsis Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron by : Edward F. Whittle

Download or read book Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron written by Edward F. Whittle and published by . This book was released on 1954 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron

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ISBN 13 :
Total Pages : 51 pages
Book Rating : 4.:/5 (78 download)

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Book Synopsis Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron by : Edward F. Whittle

Download or read book Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron written by Edward F. Whittle and published by . This book was released on 1954 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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ISBN 13 :
Total Pages : 110 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis 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 by : George L. Pratt

Download or read book 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 written by George L. Pratt and published by . This book was released on 1952 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01 by : Douglas R. Lord

Download or read book Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01 written by Douglas R. Lord and published by . This book was released on 1957 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.

Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration by : Paul L. Coe

Download or read book Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration written by Paul L. Coe and published by . This book was released on 1979 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Longitudinal Wings Position on the Pressure Characteristics at Transonic Speeds of a 45© Sweptback Wing-fuselage Model

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Effect of Longitudinal Wings Position on the Pressure Characteristics at Transonic Speeds of a 45© Sweptback Wing-fuselage Model by : William Solomon

Download or read book Effect of Longitudinal Wings Position on the Pressure Characteristics at Transonic Speeds of a 45© Sweptback Wing-fuselage Model written by William Solomon and published by . This book was released on 1953 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds by : Richard E. Kuhn

Download or read book Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds written by Richard E. Kuhn and published by . This book was released on 1955 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 by : Carl R. Jacobsen

Download or read book Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 written by Carl R. Jacobsen and published by . This book was released on 1953 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration by : P. L. Coe (Jr)

Download or read book Effects of Wing Leading-edge Deflection on Low-speed Aerodynamic Characteristics of a Low-aspect-ratio Highly Swept Arrow-wing Configuration written by P. L. Coe (Jr) and published by . This book was released on 1979 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing by : Donald E. Hewes

Download or read book The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing written by Donald E. Hewes and published by . This book was released on 1951 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.

Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model by : Byron M. Jaquet

Download or read book Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model written by Byron M. Jaquet and published by . This book was released on 1953 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics in Sideslip of a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics in Sideslip of a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge by : H. Clyde McLemore

Download or read book Aerodynamic Characteristics in Sideslip of a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge written by H. Clyde McLemore and published by . This book was released on 1958 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

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ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 by : Emma Jean Landrum

Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination by : Harold S. Johnson

Download or read book Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination written by Harold S. Johnson and published by . This book was released on 1953 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds by : Robert H. Neely

Download or read book Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds written by Robert H. Neely and published by . This book was released on 1959 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Air-flow characteristics behind wings and wing-body combinations are described and are related to the downwash at specific tail locations for unseparated and separated flow conditions. The effects of various parameters and control devices on the air-flow characteristics and tail contribution are analyzed and demonstrated. An attempt has been made to summarize certain data in a form useful for design. The experimental data herein were obtained mostly at Reynolds numbers greater than 4 x 105 and at Mach numbers less than 0.25.