Piezo-stack vortex generators for boundary layer control of a delta wing micro-aerial vehicle-Reference-Cited by-同舟云学术

Piezo-stack vortex generators for boundary layer control of a delta wing micro-aerial vehicle

Published:2013-11 Issue:2 Volume:40 Page:783-790
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Mystkowski Arkadiusz

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference22 articles.

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3. The control of flow separation by periodic excitation;Greenblatt;Prog. Aerosp. Sci.,2000

4. Use of periodic excitation to enhance airflow performance at low Reynolds numbers;Greenblatt;J. Aircr.,2001

5. Subharmonics and vortex merging in mixing layers;Ho;J. Fluid Mech.,1982

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