Wind-tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 degree swept wing airplane

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (17 download)

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Book Synopsis Wind-tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 degree swept wing airplane by : Curt A. Holzhauser

Download or read book Wind-tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 degree swept wing airplane written by Curt A. Holzhauser and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Tests of a Leading-edge Area Suction on a Fighter-type Airplane with a 35 Degree Sweptback Wing

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Flight Tests of a Leading-edge Area Suction on a Fighter-type Airplane with a 35 Degree Sweptback Wing by : Richard S. Bray

Download or read book Flight Tests of a Leading-edge Area Suction on a Fighter-type Airplane with a 35 Degree Sweptback Wing written by Richard S. Bray and published by . This book was released on 1955 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a leading-edge area-suction boundary-layer-control system, and to investigate the possible operational limitations imposed on a fighter-type airplane by such an installation. The results of the flight tests are compared with those of full-scale wind-tunnel tests of a similar installation on a model incorporating F-86 wing panels. The basic porous-area distribution tested extended the full length of the wing leading edge. Suction power was provided by a modified turbosupercharger which was driven by air bled from the compressor of the airplane's jet engine.

Research Abstracts and Reclassification Notice

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ISBN 13 :
Total Pages : 716 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Research Abstracts and Reclassification Notice by : United States. National Advisory Committee for Aeronautics

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 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Boundary Layer Theory

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ISBN 13 :
Total Pages : 684 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Boundary Layer Theory by : Hermann Schlichting

Download or read book Boundary Layer Theory written by Hermann Schlichting and published by . This book was released on 1960 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:

34th Aerospace Sciences Meeting & Exhibit

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ISBN 13 :
Total Pages : 764 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 34th Aerospace Sciences Meeting & Exhibit by :

Download or read book 34th Aerospace Sciences Meeting & Exhibit written by and published by . This book was released on 1996 with total page 764 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering Index

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ISBN 13 :
Total Pages : 1092 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aeronautical Engineering Index by :

Download or read book Aeronautical Engineering Index written by and published by . This book was released on 1955 with total page 1092 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerospace Engineering Index

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ISBN 13 :
Total Pages : 642 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Aerospace Engineering Index by :

Download or read book Aerospace Engineering Index written by and published by . This book was released on 1959 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Flight and Wind Tunnel Investigation of the Effect of Angle-of-attack Rate on Maximum Lift Coefficient

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Flight and Wind Tunnel Investigation of the Effect of Angle-of-attack Rate on Maximum Lift Coefficient by : Fox Conner

Download or read book A Flight and Wind Tunnel Investigation of the Effect of Angle-of-attack Rate on Maximum Lift Coefficient written by Fox Conner and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices

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

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Book Synopsis Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices by : W. Kreuger

Download or read book Wind Tunnel Investigations on a 35 Degree Swept-back Wing with Different High-lift Devices written by W. Kreuger and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

National Union Catalog

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ISBN 13 :
Total Pages : 622 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis National Union Catalog by :

Download or read book National Union Catalog written by and published by . This book was released on 1970 with total page 622 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes entries for maps and atlases.

Lockheed Georgia Quarterly

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Lockheed Georgia Quarterly by :

Download or read book Lockheed Georgia Quarterly written by and published by . This book was released on 1968 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A History of Suction-Type Laminar-Flow Control with Emphasis on Flight Research

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Publisher : CreateSpace
ISBN 13 : 9781493794324
Total Pages : 86 pages
Book Rating : 4.7/5 (943 download)

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Book Synopsis A History of Suction-Type Laminar-Flow Control with Emphasis on Flight Research by : National Aeronautics and Space Administration

Download or read book A History of Suction-Type Laminar-Flow Control with Emphasis on Flight Research written by National Aeronautics and Space Administration and published by CreateSpace. This book was released on 2013-11 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laminar-flow control is an area of aeronautical research that has a long history at NASA's Langley Research Center, Dryden Flight Research Center, their predecessor organizations, and elsewhere. In this monograph, Albert L. Braslow, who spent much of his career at Langley working with this research, presents a history of that portion of laminar-flow technology known as active laminar-flow control, which employs suction of a small quantity of air through airplane surfaces. This important technique offers the potential for significant reduction in drag and, thereby, for large increases in range or reductions in fuel usage for aircraft. For transport aircraft, the reductions in fuel consumed as a result of laminar-flow control may equal 30 percent of present consumption. Given such potential, it is obvious that active laminar-flow control with suction is an important technology. In this study, the author covers the early history of the subject and brings the story all the way to the mid-1990s with an emphasis on flight research, much of which occurred at Dryden.

Wind Tunnel Investigations on a 35 Degrees Swept-back Wing with Different High-lift Devices

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

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Book Synopsis Wind Tunnel Investigations on a 35 Degrees Swept-back Wing with Different High-lift Devices by : W. Kreuger

Download or read book Wind Tunnel Investigations on a 35 Degrees Swept-back Wing with Different High-lift Devices written by W. Kreuger and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Supersonic Wind Tunnel Tests of Ring-wing Configurations

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Supersonic Wind Tunnel Tests of Ring-wing Configurations by : Leon H. Schindel

Download or read book Supersonic Wind Tunnel Tests of Ring-wing Configurations written by Leon H. Schindel and published by . This book was released on 1958 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 984 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 984 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 960 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1981 with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody by : Kenneth W. Mort

Download or read book Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody written by Kenneth W. Mort and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: