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Author : Eric C. Stewart
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Parametric Study of Accelerations of an Airplane Due to a Wake Vortex System written by Eric C. Stewart and published by . This book was released on 1999 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration
Publisher :
ISBN 13 : 9781726156936
Total Pages : 40 pages
Book Rating : 4.1/5 (569 download)
Download or read book A Parametric Study of Accelerations of an Airplane Due to a Wake Vortex System written by National Aeronautics and Space Administration and published by . This book was released on 2018-08-27 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted using strip theory to systematically investigate the effects of progressively more complete descriptions of the interaction of an airplane with a wake vortex system. The emphasis was in roll-dominant, parallel, vortex encounters. That is, the simulated airplane's longitudinal axis was nearly parallel to the rotation axis of the vortex system for most of the results presented. The study began with a drag-less rectangular wing in the flow field of a single vortex and progressed to a complete airplane with aerodynamic surfaces possessing taper, sweep, dihedral, and stalling and immersed in the flow field of a vortex pair in ground effect. The effects of the pitch, roll, and yaw attitudes of the airplane on the calculated accelerations were also investigated. The airplane had the nominal characteristics of a Boeing 757, and the vortex flow field had the nominal characteristics of the wake of a Boeing 767. The Bumham-Hallock model of a vortex flow field was used throughout the study. The data are presented mainly in terms of contours of equal acceleration in a two-dimensional area centered on the vortex pair and having dimensions of 300 feet by 300 feet.Stewart, Eric C.Langley Research CenterAERODYNAMICS; FLOW DISTRIBUTION; RECTANGULAR WINGS; ROLL; ROTATION; VORTICES; YAW; AIRCRAFT WAKES; MATHEMATICAL MODELS; BOEING 757 AIRCRAFT; BOEING 767 AIRCRAFT; GROUND EFFECT (AERODYNAMICS)...
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ISBN 13 :
Total Pages : 182 pages
Book Rating : 4.:/5 (317 download)
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ISBN 13 :
Total Pages : 1248 pages
Book Rating : 4.:/5 (89 download)
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1984 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)
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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)
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ISBN 13 :
Total Pages : 228 pages
Book Rating : 4.:/5 (3 download)
Download or read book Development of a Laser Doppler System for the Detection, Tracking, and Measurement of Aircraft Wake Vortices written by and published by . This book was released on 1975 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 1004 pages
Book Rating : 4.:/5 (319 download)
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Author : Robert C. Nelson
Publisher :
ISBN 13 :
Total Pages : 464 pages
Book Rating : 4.3/5 (91 download)
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by . This book was released on 1998 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt: This 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.
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ISBN 13 :
Total Pages : 1252 pages
Book Rating : 4.:/5 (31 download)
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Author : Thomas R. Yechout
Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based 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.
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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (317 download)
Download or read book Wake Vortex Encounter Hazards Criteria for Two Aircraft Classes written by and published by . This book was released on 1976 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 636 pages
Book Rating : 4.:/5 (26 download)
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ISBN 13 :
Total Pages : 1220 pages
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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (317 download)
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Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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ISBN 13 :
Total Pages : 614 pages
Book Rating : 4.3/5 (243 download)
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ISBN 13 :
Total Pages : 612 pages
Book Rating : 4.:/5 (319 download)
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