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Latest revision as of 07:50, 12 July 2021
Abstract
In this presentation, I will first introduce some recent work on the various ways to control the unsteady wing load induced by gust encounter. This is crucially important for the safety of future civil aviation. In addition, the effective alleviation of gust load can also potentially pave the way for a significant reduction of aircraft fuel consumption through reduced structural weight and therefore drag. Since no practical wing is rigid, this leads to a strongly-coupled problem between the wing aerodynamics and its structure under the unsteady gust load. The solution of this coupled problem will discussed in some detail, including the analysis of the unsteady gust response without and with flow control.
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Published on 12/07/21
Submitted on 12/07/21
Volume IS33 - Numerical solutions of Coupled Problems Arising from Concerns about the Environmental Climate Impact, Safety, Impact on Global Health Related to International Air Transport, 2021
DOI: 10.23967/coupled.2021.060
Licence: CC BY-NC-SA license
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