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J-GLOBAL ID:200902160405425024   Reference number:02A0248241

Experimental Study of Shock Wave Fluctuation on a Circular Arc Airfoil in Transonic Flow.

遷音速流中の対称円弧翼における衝撃波変動
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Volume: 68  Issue: 666  Page: 338-343  Publication year: Feb. 25, 2002 
JST Material Number: F0036B  ISSN: 0387-5016  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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High-speed aerodynamics 
Reference (9):
  • MCDEVITT, J. B. Transonic Flow about a Thick Circular-Arc Airfoil. AIAA J. 1976, 14, 5, 606-613
  • LEE, B. H. K. Oscillating Shock Motion Caused by Transonic Shock Boundary Layer Interaction. AIAA J. 1990, 17, 10, 1076-1083
  • BOGAR, T. J. Structure of Self-Excited Oscillation in Tran-sonic Diffuser Flows. AIAA J. 1986, 24, 1, 54-61
  • YAMAMOTO, K. Self-Excited Oscillation of Shock Waves on an Airfoil in Twodimensional Transonic Channel Flows. Proceedings of 4^<th> Symposium on Unsteady Aerodynamics and Aeroelasiticity of Turbomachines and Propellers. 1987, 763-783
  • ARAKI, T. Self-Excited Flow Oscillation in the Low Pressure Steam Turbine Cascade. Proceedings of the IUTAM Symposium, 'Aeroelasiticity in Turbomachines'. 1980
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