Approach to determine the circulation and vorticity around supersonic airfoil with spoiler
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Aerospace Engineering,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42401-023-00244-3.pdf
Reference19 articles.
1. Abrar H, Masudar R, Ashabul H (2021) Theoretical study of mach number and compressibility effect on the slender airfoils. Appl Appl Math 16(1):30
2. Ansari SA, Zbikowski R, Knowles K (2006) A non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: implementation and validation. Proc Inst Mech Eng Part G 30(2):169–186. https://doi.org/10.1243/09544100JAERO50
3. Batchelor GK (1967) An introduction to fluid dynamics. Cambridge University Press, p 615
4. Bisplinghoff RL, Ashley H, Halfman RL (1996) Aeroelasticity. Dover Publications
5. Chang C, Hsiau Y, Chu C (1993) Starting vortex and lift on an airfoil. Physics of fluid 5(11):2826–2830. https://doi.org/10.1063/1.858745
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