Proceedings of the KSME Conference (대한기계학회:학술대회논문집)
- 2002.08a
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- Pages.795-798
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- 2002
A Computational Study of the Vortical Flows over a Delta Wing At High-Angle of Attack
고영각의 델타익에서 발생하는 와유동에 관한 수치해석적 연구
- Published : 2002.08.01
Abstract
This paper dispicts the vortical flow characteristics over a delta wing using a computational analysis for the purpose of investigating and visualizing the effect of the angle of attack and fee stream velocity on the low-speed delta wing aerodynamics. Computations are applied to the full, 3-dimensional, compressible, Navier-Stokes Equations. In computations, the free stream velocity is changed between 20m/s and 60m/s and the angle of attack of the delta wing is changed between
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