Quantitative Visualization of the Leading-edge Vortices on a Delta Wing by Using Pressure-sensitive Paint

Journal of Visualization

Volumn 4, Issue 2, 2001, Pages 139-150

  Egami, Y ^a   Lijima, Y ^a   Amao, Y ^a   Asai, K ^a   Fuji, A ^b   Teduka, N ^b   Kameda, M ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO UNIVERSITY OF AGRICULTURE AND TECHNOLOGY   (Japan)

Author keywords

Delta wing; Image analysis; Leading edge vortices; Pressure sensitive paint; Vortex breakdown

Indexed keywords

EID: 23044526039     PISSN: 13438875     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF03182567     Document Type: Article

References (6)

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2. Elsenaar, A., Hjelmberg, L. and Buetefisch, K., The International Vortex Flow Experiment, AGARD CP-437, Paper 9, (1988).
3. Liu, T., Guille, M. and Sullivan, J. P., Uncertainty Analysis of Pressure Sensitive Paint Measurement, AIAA Paper 99-3785 (1999).
4. Liu, T., Campbell, B. T., Burns, S. P. and Sullivan, J. P., Temperature and Pressure-Sensitive Luminescent Paints in Aerodynamics, Apl. Mech. Rev., 50-4 (1997), 227-246.
5. Shimbo, Y., Mehta, D. R. and Cantwell, J. B., Vortical Flow Field Investigation Using the Pressure Sensitive Paint Technique at Low Speed, AIAA Paper 97-0388 (1997).
6. Shimbo, Y., Asai, K., Kanda, H., Iijima, I., Komatu, N., Kita, S. and Ishiguro, M., Evaluation of Several Calibration Techniques for Pressure Sensitive Paint in Transonic Testing, AIAA Paper 98-2502 (1998).