Influence Of Flight Control Laws On Structural Sizing Of Commercial Aircraft
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Influence of flight control laws on structural sizing of commercial aircraft
Author | : Rahmetalla Nazzeri |
Publsiher | : Cuvillier Verlag |
Total Pages | : 180 |
Release | : 2021-11-15 |
Genre | : Technology & Engineering |
ISBN | : 9783736965164 |
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The increasing demand for new civil aircraft pushes aircraft manufacturers to develop innovative solutions that lead in particular to mass reductions. One way to achieve these kinds of improvements is the use of multidisciplinary analysis and optimization. In this sense the intention of this PhD thesis is to develop a multidisciplinary framework in order to quantify the impact of load alleviation function parameter changes on structural components like the wing and fuselage in terms of resulting mass changes. The developed iterative process chain covers the loads calculation including an active load alleviation system, a structural assessment of the wing and fuselage components and a dedicated feedback loop in order to update mass and stiffness properties of the loads calculation model. The study shows that significant mass reductions are achievable while on the other hand estimated mass penalties are irrelevant.
Airbus Flight Control Laws
Author | : Bill Palmer |
Publsiher | : William Palmer |
Total Pages | : 135 |
Release | : 2017-06-30 |
Genre | : Transportation |
ISBN | : 9780989785730 |
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An exploration of the Airbus fly-by-wire flight control laws that become active when Normal law can no longer function. A follow on to Airbus A330 Normal Law.
Flight Stability and Automatic Control
Author | : Robert C. Nelson |
Publsiher | : WCB/McGraw-Hill |
Total Pages | : 441 |
Release | : 1998 |
Genre | : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite |
ISBN | : 0071158383 |
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The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Structural Loads Analysis
Author | : Ted L. Lomax |
Publsiher | : AIAA |
Total Pages | : 306 |
Release | : 1996 |
Genre | : Airframes |
ISBN | : 1600861180 |
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The Application of a C Flight Control Law to a Large Civil Transport Aircraft
Author | : Edmund J. Field,Cranfield Institute of Technology. College of Aeronautics |
Publsiher | : Unknown |
Total Pages | : 36 |
Release | : 1993 |
Genre | : Aeronautics |
ISBN | : 1871564581 |
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Scientific and Technical Aerospace Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 702 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : UIUC:30112048646605 |
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Applied Mechanics Reviews
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 620 |
Release | : 1996 |
Genre | : Mechanics, Applied |
ISBN | : UIUC:30112046051139 |
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Aeroplane and Commercial Aviation News
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 574 |
Release | : 1962 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105117452370 |
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