SIMULATION OF PITCHING AND HEAVING AIRFOIL WITH OSCILLATION OF FLOW BOUNDARY CONDITION

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DJAVARESHKIAN M.H.; FAGHIHI A.M.

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Paper Information

Journal: Journal of Aerospace Science and Technology Year:2013 | Volume:10 | Issue:1 Page(s): 27-37

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Title

SIMULATION OF PITCHING AND HEAVING AIRFOIL WITH OSCILLATION OF FLOW BOUNDARY CONDITION

Author(s)

DJAVARESHKIAN M.H. | FAGHIHI A.M. | Issue Writer Certificate

Keywords

PITCHING

HEAVING

TRANSONIC

INVISCID

VISCOUS

BOUNDARY CONDITION

Abstract

A pressure based implicit procedure to solve the Euler and Navier-Stokes equations is developed to predict TRANSONIC VISCOUS and INVISCID flows around the PITCHING and HEAVING airfoils with a high resolution scheme. In this process, no northogonal and non moving mesh with collocated finite volume formulation are used. In order to simulate PITCHING or HEAVING airfoil, oscillation of flow BOUNDARY CONDITION is applied. The boundedness criteria for this procedure are determined from Normalized Variable Diagram (NVD) scheme. The procedure incorporates the k- e eddy-viscosity turbulence model. This process is tested for INVISCID and turbulent TRANSONIC aerodynamic flows around oscillation airfoil. The results are compared with other existing numerical solutions and with the experimental data. The comparisons show that the resolution quality of the developed algorithm is significant.

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APA: Copy

DJAVARESHKIAN, M.H., & FAGHIHI, A.M.. (2013). SIMULATION OF PITCHING AND HEAVING AIRFOIL WITH OSCILLATION OF FLOW BOUNDARY CONDITION. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), 10(1), 27-37. SID. https://sid.ir/paper/291007/en

Vancouver: Copy

DJAVARESHKIAN M.H., FAGHIHI A.M.. SIMULATION OF PITCHING AND HEAVING AIRFOIL WITH OSCILLATION OF FLOW BOUNDARY CONDITION. JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST)[Internet]. 2013;10(1):27-37. Available from: https://sid.ir/paper/291007/en

IEEE: Copy

M.H. DJAVARESHKIAN, and A.M. FAGHIHI, “SIMULATION OF PITCHING AND HEAVING AIRFOIL WITH OSCILLATION OF FLOW BOUNDARY CONDITION,” JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST), vol. 10, no. 1, pp. 27–37, 2013, [Online]. Available: https://sid.ir/paper/291007/en

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