THE LOW FREQUENCY OSCILLATION IN THE FLOW OVER A NACA0012 AIRFOIL WITH AN LEADING EDGE | 東京工業大学附属図書館文献データベース

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THE LOW FREQUENCY OSCILLATION IN THE FLOW OVER A NACA0012 AIRFOIL WITH AN LEADING EDGE

著者名:: Zaman, K. B.M.Q. et al. ( NASA. Lewis Research Center )
掲載資料名:: NASA Technical Reports(N89)
発行年:: 1989
号:: NASA-TM-102018
通号:: G3/02 0210311
パート:: NAS1.15:102018
ペーパー番号:: N89-23417
開始ページ:: 1
終了ページ:: 16
総ページ数:: 16
出版情報:: National Aeronautics and Space Administration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:

ZA00001425

類似資料:

1 テクニカルペーパー A NATURAL LOW FREQUENCY OSCILLATION IN THE WAKE OF AN AIRFOIL NEAR STALLING CONDITIONS Zaman, K. B.M.Q. et al. National Aeronautics and Space Administration	7 テクニカルペーパー A Quantiative Comparison of Leading-Edge Vortices in Incompressible and Supersonic Flows. Wang, F.Y., Milanovic, I.M., Zaman, K.B.M. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー CONTROL OF LAMINAR SEPARATION OVER AIRFOILS BY ACOUSTIC EXCITATION Zaman, K. B.M.Q. et al. National Aeronautics and Space Administration	8 テクニカルペーパー A FLOW VISUALIZATION STUDY OF THE LEADING EDGE SEPARATION BUBBLE ON A NACA 0012 AIRFOIL WITH SIMULATED GLAZE ICE Khodadoust, Abdollah National Aeronautics and Space Administration
3 テクニカルペーパー Examination of the Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil D. Sahoo., R. Srinivasan., R. Bowersox American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Prediction of Oscillatory Flow Excitation at the Leading Edge of a Modified NACA 0015 Airfoil Yazzie, R., Salari, K. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Jet noise reduction by microjets- A parametric study Zaman, K. B.M.Q. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Experimental investigation of the flowfield of an oscillating airfoil Panda, J., Zaman, K. B. M. Q. National Aeronautics and Space Adminstration
5 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	11 テクニカルペーパー Numerical Simulation of NACA0012 Wingtip Flow Leading to Noise Generation Imamura, T., Enomoto, S., Kato, H., Yokokawa, Y., Yamamoto, K. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Effect of Acoustic Excitation on Stalled Flows Over an Airfoil Zaman, K.B.M.Q. National Aeronautics and Space Adminstration	12 テクニカルペーパー An Experimental and Theoretical Study of Transonic Flow About the NACA 0012 Airfoil B. Rasuo American Institute of Aeronautics and Astronautics

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