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Investigation and Wind Tunnel Test on Gust Load Alleviation for a Flying Wing

  • Beihang University
  • CAS - Institute of Mechanics

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Based on the latest developments in gust alleviation technology, this paper studies and establishes the modeling methods, control scheme design and practical alleviation methods for gust alleviation techniques. The effectiveness of the modeling method and the gust alleviation control scheme was verified by wind tunnel tests.

Original languageEnglish
Title of host publicationProceedings of the 6th China Aeronautical Science and Technology Conference - Volume 3
PublisherSpringer Science and Business Media Deutschland GmbH
Pages550-558
Number of pages9
ISBN (Print)9789819988662
DOIs
StatePublished - 2024
Event6th China Aeronautical Science and Technology Conference, CASTC 2023 - Wuzhen, China
Duration: 26 Sep 202327 Sep 2023

Publication series

NameLecture Notes in Mechanical Engineering
ISSN (Print)2195-4356
ISSN (Electronic)2195-4364

Conference

Conference6th China Aeronautical Science and Technology Conference, CASTC 2023
Country/TerritoryChina
CityWuzhen
Period26/09/2327/09/23

Keywords

  • flying wing
  • gust load alleviation
  • wind tunnel test

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