Technical Abstract Bulletin
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Published:
Total Pages: 1048
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Published: 1980
Total Pages: 1280
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Published: 1993
Total Pages: 1448
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Published: 1979
Total Pages: 1324
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Published: 1980-03
Total Pages: 172
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DOWNLOAD EBOOKAuthor: Robert C. Nelson
Publisher:
Published: 1998
Total Pages: 464
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DOWNLOAD EBOOKThis edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: National Aeronautics and Space Administration
Publisher: CreateSpace
Published: 2013-11
Total Pages: 86
ISBN-13: 9781493794324
DOWNLOAD EBOOKLaminar-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.
Author: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author: Donald L. Loving
Publisher:
Published: 1966
Total Pages: 20
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Published: 1979
Total Pages: 8
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