Synthetic jets influence on NACA 0012 airfoil at high angles of attack

Synthetic jets influence on NACA 0012 airfoil at high angles of attack

著者名:: Nae, Catalin ( National Institute for Aerospace Research "Elie Carafoli", Romania )
掲載資料名:: A collection of technical papers : AIAA Atmospheric Flight Mechanics Conference and Exhibit, August 10-12, 1998/Boston, Massachusetts
シリーズ名:: AIAA Paper : AIAA Atmospheric Flight Mechanics Conference
シリーズ巻号:: CP9808
発行年:: 1998
通号:: 98-4523
ペーパー番号:: AIAA 98-4523
開始ページ:: 854
終了ページ:: 859
出版情報:: Reston VA: American Institute of Aeronautics and Astronautics
ISBN:: 9781563472701 [1563472708]
言語:: 英語
請求記号:: A07400/9808
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:	ZA00003930
シリーズID:	PA00000162
会議名:	AIAA Atmospheric Flight Mechanics Conference and Exhibit
回次:	1998
会議開催地:	Boston, Massachusetts
会議開催年:	1998.08.10-1998.08.12

類似資料:

1 テクニカルペーパー Unsteady Flow Control Using Synthetic Jet Actuators Nae, Catalin American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Impulsive Start of a Symmetric Airfoil at High Angle of Attack Katz, Joseph, Yon, Steven, Rogers, Stuart E. National Aeronautics and Space Adminstration
2 テクニカルペーパー Effect of zero-mass "synthetic" jets on the aerodynamics of the NACA-0012 airfoil Hassan, Ahmed A., JanakiRam, Ram D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー HIGH REYNOLDS NUMBER TRANSONIC TESTS ON A NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Ladson, Charies L. et al. National Aeronautics and Space Administration
3 テクニカルペーパー Application of Co-Flow Jet Concept on Thin Airfoil at High Angle of Attack A. Rachman, H. Tsai, G. Zha American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Flow Solver And Anisotropic Mesh Adaption Using A Change of Metric Based on Flow Variables Nae, Catalin American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Detached-eddy simulation of a co-flow jet airfoil at high angle of attack Wang, Baoyuan, Zha, Ge-Cheng American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Wind tunnel data analysis using image processing Nae, Catalin American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Multiphase Flow with Convective Droplet Impact on a NACA Airfoil at Varying Angles of Attack X. Wang, E. Bibeau, G. Naterer American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Numerical Investigation of Transitional Flows over a NACA0012 Airfoil. Alam, M., Suzen, Y.B. Society of Automotive Engineers
6 テクニカルペーパー Effects of Synthetic Jet Actuation on a Pitching NACA 0015 Airfoil Traub, L., Miller, A., Rediniotis,O. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー PRESSURE DISTRIBUTIONS FROM HIGH REYNOLDS NUMBER TRANSONIC TESTS OF AN NACA 0012 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL Ladson, Charies L. et al. National Aeronautics and Space Administration

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