Open Access
| Issue |
EPJ Web Conf.
Volume 180, 2018
EFM17 – Experimental Fluid Mechanics 2017
|
|
|---|---|---|
| Article Number | 02080 | |
| Number of page(s) | 7 | |
| Section | Contributions | |
| DOI | https://doi.org/10.1051/epjconf/201818002080 | |
| Published online | 04 June 2018 | |
- Heron, I., & Myose, R. Y. On the impingement of a von kàrmàn vortex street on a delta wing. Collection of Technical Papers - AIAA 22nd Applied Aerodynamics Conference, 1 178-188 (2004). [Google Scholar]
- Su, W., Liu, M., & Liu, Z. Topological structures of separated flows about a series of sharp-edged delta wings at angles of attack up to 90°. Topological Fluid Mechanics, edited by H. K. Moffatt, and A. Tsinober, Cambridge Univ. Press, New York (1990). [Google Scholar]
- NASA, (2016). Jet Exit Facility-Bubble Type Vortex Breakdown and Spiral Type Vortex Breakdown. https://crgis.ndc.nasa.gov/historic/Jet_Exit_Facility [Google Scholar]
- Sarpkaya, T. On stationary and travelling vortex breakdowns. Journal of Fluid Mechanics, 45(3), 545-559. doi:10.1017/S0022112071000181 (1971). [Google Scholar]
- Yayla, S., Canpolat, C., Sahin, B., & Akilli, H. The effect of angle of attack on the flow structure over the nonslender lambda wing. Aerospace Science and Technology, 28 (1), 417-430. doi:10.1016/j.ast.2012.12.007 (2013). [Google Scholar]
- Sahin, B., Yayla, S., Canpolat, C., & Akilli, H. Flow structure over the yawed nonslender diamond wing. Aerospace Science and Technology, 23(1), 108-119. doi:10.1016/j.ast.2011.06.008 (2012). [Google Scholar]
- Karasu, I. Effect of yaw angle on vortex formation over a slender delta wing. Qukurova University Institute of Natural and Applied Sciences, Ph. D. Thesis, Adana, 159p (2015). [Google Scholar]
- Woodiga, S., Liu, T., Ramasamy, R. S. V., & Kode, S. K. Effects of pitch, yaw, and roll on delta wing skin friction topology. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 230(4), 639-652. doi:10.1177/0954410015594823 (2016). [CrossRef] [Google Scholar]
- Canpolat, C., Sahin, B., Yayla, S., & Akilli, H. Effects of perturbation on the flow over nonslender delta wings. 45th AIAA Fluid Dynamics Conference, 1-10 (2015) [Google Scholar]
- Ozgoren, M., & Sahin, B. (2002). Effect of pitching delta wing on vortex structures with and without impingement plate. Turkish J. Eng. Env. Sci., 26, 325-343. [Google Scholar]
- LeMay, S. P., Batill, S. M., & Nelson, R. C. (1990). Vortex dynamics on a pitching delta wing. Journal of Aircraft, 27(2), 131-138. doi:10.2514/3.45908 [Google Scholar]
- Canpolat C., Yayla S., Sahin B., Akilli H., “Effects of Trailing-Edge Attachment on the Flow Structure over a Generic Delta Wing” Journal of Aerospace Engineering 30, 06017003, 2017 [Google Scholar]
- Yayla S., Canpolat C., Sahin B., Akilli H.,“ Yaw Angle Effect on Flow Structure over the Nonslender Diamond Wing” AIAA JOURNAL, Vol.48, No.10,pp2457-2461,2010 [Google Scholar]
- Canpolat C., Yayla S., Sahin B., “Observation of the Vortical Flow over a Yawed Delta Wing”, Journal of Aerospace Engineering, Vol. 25, Issue. 4, pp. 613626, 2012 [Google Scholar]
- Canpolat C., Yayla S., Sahin B., Akilli H., “Dye Visualization of the Flow Structure over a Yawed Nonslender Delta Wing” Journal of Aircraft, Vol. 46, No.5, September-October 2009. [Google Scholar]
- Karasu, I, Tasci M., O., Sahin, B., and Akilli H., Stereo PIV investigation on windward side leading edge vortex of a yawed slender delta wing, Conferences on Advances in Mechanical Engineering, 11-13 May 2016, Yildiz Technical University, Istanbul, Turkey [Google Scholar]
- Sahin, B., Taşcı., M., O.,, Karasu, I., Akıllı H., Flow structures in end-view plane of slender delta wing, Experimental Fşuid Mechanics 2016, November 15-18, 2016 Czech Republic [Google Scholar]
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