Download or read book Blowing Over the Flaps and Wing Leading Edge of a Thin 49 Degree Swept Wing body tail Configuration in Combination with Leading edge Devices written by H. Clyde McLemore and published by . This book was released on 1956 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley full-scale tunnel to determine the effects on the low-speed aerodynamic characteristics of blowing air over the trailing-edge flap of a large-scale wing-body-tail model. The wing and horizontal tail have an aspect ratio of 3.5, taper ratio of 0.3, leading-edge sweep of 49 degrees, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The trailing-edge air was ejected over highly deflected half- and full-span flaps in combination with several leading-edge-flow control devices including blowing from a slot in the wing leading edge. The momentum coefficient range was investigated was 0 to 0.16 for the trailing-edge blowing and 0 to 0.025 for the leading-edge blowing. Most of the tests were conducted at a Reynolds number of 5,200,000 corresponding to a Mach number of 0.08.

Download or read book High pressure Blowing Over Flap and Wing Leading Edge of a Large scale 49 Degrees Swept Wing body tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase written by Marvin P. Fink and published by . This book was released on 1957 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High pressure Blowing Over Flap and Wing Leading Edge of a Thin Large scale 49 Swept Wing body tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase written by Marvin P. Fink and published by . This book was released on 1957 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High pressure Blowing Over Flap and Wing Leading Edge of a Thin Large scale 49 Degree Swept Wing body tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase written by Marvin P. Fink and published by . This book was released on 1957 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 49 degree swept-wing complete model equipped for high-pressure blowing full span at two chordwise locations at the leading edge of a full-span wing and over a half-span flap has been tested in the Langley full-scale tunnel to determine the effectiveness of blowing at the leading edge as a supplementary leading-edge stall control at high lift coefficients.

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.

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

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:

Download or read book Surface Pressure Distributions on 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 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Surface Pressure Distributions on a Large scale 49 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 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Leading edge Devices and Trailing edge Flaps on Longitudinal Characteristics of Two 47 7 Degrees Sweptback Wings of Aspect Ratios 5 1 and 6 0 at a Reynolds Number of 6 0 X 10 6 written by Reino J. Salmi and published by . This book was released on 1950 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Aerodynamic Characteristics of a Large Scale Unswept Wing Body Tail Configuration with Blowing Applied Over the Flap and Wind Leading Edge written by and published by . This book was released on 1960 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 swept Wing written by William P. Henderson and published by . This book was released on 1978 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Blowing type Boundary layer Control as Applied to the Trailing edge Flaps of a 35 Degree Swept wing Airplane written by Mark W. Kelly and published by . This book was released on 1958 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Several Leading edge Modifications on the Stalling Characteristics of a 45 Degrees Swept forward Wing written by Gerald M. McCormack and published by . This book was released on 1949 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of a Leading Edge Flap Upon the Lift Drag and Pitching Moment of an Airplane Employing a Thin Unswept Wing written by John C. Heitmeyer and published by BiblioGov. This book was released on 2013-07 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of deflecting full-span, constant-chord, leading-edge flaps, having either round or sharp leading edges, upon the lift, drag, . and pitching moment characteristics of a model of an interceptor-type aircraft have been determined experimentally at subsonic and supersonic speeds. Results indicate that the variations of lift with angle of attack and of pitching moment with lift were unaffected by either the shape of the flap leading edge or flap deflection. Deflection of the flaps having either a round or sharp leading edge increased the drag at zero lift at both subsonic and supersonic speeds. In spite of the increase in the drag at zero lift, however, deflection of the flaps increased the maximum lift-drag ratio at subsonic speeds and had no deleterious effect at supersonic speeds