Laminar Flow Aircraft Certification
Author:
Publisher:
Published: 1986
Total Pages: 340
ISBN-13:
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Author:
Publisher:
Published: 1986
Total Pages: 340
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1986
Total Pages: 322
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1986
Total Pages: 322
ISBN-13:
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Publisher:
Published: 1990
Total Pages: 54
ISBN-13:
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Publisher:
Published: 1979
Total Pages: 8
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DOWNLOAD EBOOKAuthor: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
Published: 2018-10-24
Total Pages: 28
ISBN-13: 9781729189429
DOWNLOAD EBOOKAn averaging total pressure wake rake used by the Cessna Aircraft Company in flight tests of a modified 210 airplane with a laminar flow wing was calibrated in wind tunnel tests against a five-tube pressure probe. The model generating the wake was a full-scale model of the Cessna airplane wing. Indications of drag trends were the same for both instruments. Irani, E. and Snyder, M. H. Unspecified Center RTOP 505-61-41-02
Author: E. Irani
Publisher:
Published: 1988
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKAuthor: Philip P. Antonatos
Publisher:
Published: 1964
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: R.W. Barnwell
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 415
ISBN-13: 1461228727
DOWNLOAD EBOOKResearch on laminar flow and its transition to turbulent flow has been an important part of fluid dynamics research during the last sixty years. Since transition impacts, in some way, every aspect of aircraft performance, this emphasis is not only understandable but should continue well into the future. The delay of transition through the use of a favorable pressure gradient by proper body shaping (natural laminar flow) or the use of a small amount of suction (laminar flow control) was recognized even in the early 1930s and rapidly became the foundation of much of the laminar flow research in the U.S. and abroad. As one would expect, there have been many approaches, both theoretical and experimental, employed to achieve the substantial progress made to date. Boundary layer stability theories have been formu lated and calibrated by a good deal of wind tunnel and flight experiments. New laminar now airfoils and wings have been designed and many have been employed in aircraft designs. While the early research was, of necessity, concerned with the design of subsonic aircraft interest has steadily moved to higher speeds including those appropriate to planetary entry. Clearly, there have been substantial advances in our understanding of transition physics and in the development and application of transition prediction methodolo gies to the design of aircraft.
Author: United States. Congress. House. Committee on Public Works and Transportation. Subcommittee on Aviation
Publisher:
Published: 1994
Total Pages: 168
ISBN-13:
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