Numerical Study for Flow Behavior and Drag of Axisymmetric Boattail Models at Different Mach Number
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-1968-8_60
Reference13 articles.
1. Viswanath, P.R.: Flow management techniques for base and afterbody drag reduction. Prog. Aerosp. Sci. 32(2–3), 79–129 (1996). https://doi.org/10.1016/0376-0421(95)00003-8
2. Jagtap, K.S., Sundarraj, K., Kumar, N., Rajnarasimha, S., Kulkarni, P.S.: Numerical study of base drag reduction using locked vortex flow management technique for lower subsonic regime. Int. J. Mech. Mechatron. Eng. 12(2), 188–191 (2018). https://doi.org/10.5281/zenodo.1316596
3. Mair, W.A.: Reduction of base drag by boat-tailed afterbodies in low speed flow.pdf. Aeronaut. Q. 20, 307–320 (1969)
4. Tran, T.H., Ambo, T., Lee, T., Chen, L., Nonomura, T., Asai, K.: Effect of boattail angles on the flow pattern on an axisymmetric afterbody surface at low speed. Exp. Therm. Fluid Sci. 99, 324–335 (2018). https://doi.org/10.1016/j.expthermflusci.2018.07.034
5. Tran, T.H., Ambo, T., Chen, L., Nonomura, T., Asai, K.: Effect of boattail angle on pressure distribution and drag of axisymmetric afterbodies under low-speed conditions. Trans. Jpn. Soc. Aeronaut. Space Sci. 62(4), 219–226 (2019). https://doi.org/10.2322/tjsass.62.219
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