Aerodynamic Control of High Performance Aircraft Using Pulsed Plasma Actuators-Reference-Cited by-同舟云学术

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Aerodynamic Control of High Performance Aircraft Using Pulsed Plasma Actuators

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Matsuno Takashi¹,Kawazoe Hiromitsu¹,Nelson Robert²

Affiliation:

1. Tottori University

2. University of Notre Dame

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-697

Reference8 articles.

1. Forebody vortex control

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. HEMLAB Algorithm Applied to HIOCFD Delta Wing and OTC1 Missile;AIAA AVIATION 2023 Forum;2023-06-08

2. Feedback Flow Control: A Heuristic Approach;AIAA Journal;2018-10

3. Experimental Closed-Loop Flow Control of a von Kármán Ogive at High Incidence;AIAA Journal;2014-12

4. Efficient global optimization applied to wind tunnel evaluation-based optimization for improvement of flow control by plasma actuators;Engineering Optimization;2014-09-29

5. Closed-Loop Flow Control of a Forebody at a High Incidence Angle;AIAA Journal;2014-07

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