Approach to determine the circulation and vorticity around supersonic airfoil with spoiler

Author:

Hoque Abrar,Alam Zahangir,Hoque Ashabul

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Aerospace Engineering,Control and Systems Engineering

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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