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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2004.10
- 수록면
- 1,837 - 1,848 (12page)
이용수
초록· 키워드
오류제보하기
Interaction behaviors of high-speed compressible viscous flow and thermal-structural response of structure are presented. The compressible viscous laminar flow behavior based on the Navier-Stokes equations is predicted by using an adaptive cell-centered finite-element method. The energy equation and the quasi-static structural equations for aerodynamically heated structures are solved by applying the Galerkin finite-element method. The finite-element formulation and computational procedure are described. The performance of the combined method is evaluated by solving Mach 4 flow past a flat plate and comparing with the solution from the finite different method. To demonstrate their interaction, the high-speed flow, structural heat transfer, and deformation phenomena are studied by applying the present method to Mach 10 flow past a flat plate.
목차
Abstract
1. Introduction
2. Theoretical Formulation and Solution Procedure
3. Adaptive Meshing Technique
4. Applications
5. Concluding Remarks
Acknowledgement
References
참고문헌 (22)
참고문헌 신청
[학술지(정기간행물)] - Anderson / 1982 / Modern Compressible Flow With Historical Prospective
[학술지(정기간행물)] - Anderson / 1991 / Fundamentals of Aerodynamics
[학술지(정기간행물)] - Anderson / 1995 / Computational Fluid Dynamics
[학술지(정기간행물)] - M. J. Berger / 2000 / A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries
[학술지(정기간행물)] - Baek / 2003 / An Experimental Study of Supersonic Dual Coaxial Free Jet 17 (12) : 2107 2115 ~
[학술지(정기간행물)] - Anderson / 1991 / Fundamentals of Aerodynamics
[학술지(정기간행물)] - Anderson / 1995 / Computational Fluid Dynamics
[학술지(정기간행물)] - M. J. Berger / 2000 / A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries
[학술지(정기간행물)] - Baek / 2003 / An Experimental Study of Supersonic Dual Coaxial Free Jet 17 (12) : 2107 2115 ~
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