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Autor:
Jones, Natasha Ruth
Shock control bumps (SCBs) are considered promising flow control devices for transonic commercial aircraft. By generating a λ-shock structure, 2D SCBs offer large drag savings, but perform poorly when that structure breaks down off-design. Milder-pe
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.745050
Autor:
Jones, Natasha Ruth
Shock control bumps (SCBs) are considered promising flow control devices for transonic commercial aircraft. By generating a λ-shock structure, 2D SCBs offer large drag savings, but perform poorly when that structure breaks down off-design. Milder-pe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4460cb7bbd9227313306ef826d474c4