Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators-Reference-Cited by-同舟云学术

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Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators

Published:2005-05 Issue:3 Volume:42 Page:698-709
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Margalit S.¹,Greenblatt D.¹,Seifert A.¹,Wygnanski I.¹

Affiliation:

1. Tel-Aviv University, 69978 Tel-Aviv, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.6904

Reference39 articles.

1. Effective F+Cµ, % Re × 104Gad-el-Hak and 5.5 0.3-1.28 1.25

2. Blackwelder14Gu et al.151.3 7.7a1.7 Guy et al.19,20,231.2-1.75 1.9-2.3a2.1-55

3. Siegel et al.24,25Present investigation 1.0-4.0 0.41, 3.8 11.7 Present investigation 1.0-2.0 0.03-0.41 23.5-35.0

4. Research into vortex breakdown control

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