한국전산유체공학회:학술대회논문집
- 2007.04a
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- Pages.3-7
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- 2007
A COMPUTATIONAL STUDY ON THE CHARACTERISTICS OF ASYMMETRIC VORTEX OF TANGENT-OGIVE-CYLINDER FLIGHT VEHICLE AT HIGH ANGLES OF ATTACK
Tangent-Ogive-Cylinder 비행체의 고앙각에서의 비대칭 와류 특성 연구
Abstract
The characteristics of asymmetric vortex and side force of tangent-ogive-cylinder flight vehicle at high angles of attack have been performed by using upwind Navier-Stokes method with the
Keywords
- tangent-ogive-cylinder;
- high angles of attack;
- asymmetric vortex;
- ${\kappa}-{\omega}$ turbulent model;
- transition