Optimal disturbances in boundary layers subject to streamwise pressure gradient

Anatoli Tumin, David E. Ashpis

Research output: Contribution to journalArticle

8 Scopus citations

Abstract

The optimal disturbances/streamwise vortices associated with the transient growth mechanism was performed for boundary layers in the presence of a streamwise pressure gradient. The theory provided the optimal spacing of the control elements in the spanwise direction and their placement in the streamwise direction.

Original languageEnglish (US)
Pages (from-to)2297-2300
Number of pages4
JournalAIAA Journal
Volume41
Issue number11
Publication statusPublished - Nov 2003

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ASJC Scopus subject areas

  • Aerospace Engineering

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