Enhanced Performance of Airfoils at Moderate Mach Numbers Using Zero-Mass Flux Pulsed Blowing

Enhanced Performance of Airfoils at Moderate Mach Numbers Using Zero-Mass Flux Pulsed Blowing

著者名:

Hites,M. ( Illinois Institute of Technology )
Nagib,H. ( Tel Aviv University )
Bachar,T.
Wygnanski,I.

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2001

発行年:

2001

通号:

2001-0734

ペーパー番号:

AIAA-2001-0734

開始ページ:

1

終了ページ:

12

総ページ数:

12

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050880
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting & Exhibit
回次:	39th
会議開催地:	Reno, Nevada
会議開催年:	2001.01.08-2001.01.11
論文注記:	39th AIAA Aerospace Sciences Meeting & Exhibit 8-11 January 2001/Reno, NV

類似資料:

1 テクニカルペーパー Effective Flow Control for Rotorcraft Applications at Flight Mach Numbers (Invited) Nagib,Hassan, Kiedaisch,John, Greenblatt,David, Wygnanski,Israel, Hassan,Ahmed American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Airfoil performance enhancement using pulsed jet separation control McManus, K., Magill, J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Unsteady-Pressure Corrections in Highly Attenuated Measurements at Moderate Mach Numbers Greenblatt,David, Kiedaisch,John, Nagib,Hassan American Institute of Aeronautics and Astronautics	8 テクニカルペーパー ENHANCEMENT OF TRANSONIC AIRFOIL PERFORMANCE USING PULSED JETS FOR SEPARATION CONTROL Tilmann,Carl P. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Download Alleviation on a V-22 Model Having a Simple Flap Used in Conjunction With Periodic Excitation, Suction and Blowing. Schmalzel, M., Varghese, P., Wygnanski, I. Society of Automotive Engineers	9 テクニカルペーパー Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers M. Tamai, Z. Wang, G. Rajagopalan, H. Hu, G. He American Institute of Aeronautics and Astronautics
4 テクニカルペーパー A Review of Experimental Studies of Surface Roughness and Blowing on the Heat Transfer and Skin Friction to Nosetips and Slender Cones in High Mach Numbers … T. Wadhams, M. Holden American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Characterization of Zero Mass Flux Flow Control for Separation Control of an Adaptive Airfoil N. Pern, J. Jacob, R. Lebeau American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Numerical Simulation of the Generation of Airfoil Tones at Moderate Reynolds Numbers C. Tam, H. Ju American Institute of Aeronautics and Astronautics	11 テクニカルペーパー On the use of plasma actuators for improving the performance of airfoils J. Mabe, F. Calkings, B. Wesley, R. Woszidlo, L. Taubert, I. Wygnanski American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Drag of Shroud Deployment Bladder at Mach Numbers of 8 to 20 Panetta,A., Nagamatsu,H., Myrabo,L., Minucci,M., Messitt,D., Dominick,T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Role of Turbulent Prandtl Number on Heat Flux at Hypersonic Mach Numbers Xiao, X., Edwards, J., Hassan, H., Gaffney, R. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12