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고차 해상도와 비진동 특성을 가진 Euler 방정식 수치해법 연구 = A comparative study on high resolution and nonoscillatory schemes for euler solvers
서명 / 저자 고차 해상도와 비진동 특성을 가진 Euler 방정식 수치해법 연구 = A comparative study on high resolution and nonoscillatory schemes for euler solvers / 고덕곤.
발행사항 [대전 : 한국과학기술원, 1992].
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8002953

소장위치/청구기호

학술문화관(문화관) 보존서고

MAE 92002

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High resolution schemes for the Euler equation are studied to calculate shock-capturing and propagating wave problems. In general, monotone methods, having total variation diminishing(TVD) property and satisfing the entropy condition, are used to remove oscillatory results in the case of upwind schemes. However, they are at most first order accurate. For the higher order accuracy, two types of schemes are employed and compared. First, limiter methods based on the second order MUSCL(monotonic upstream centered scheme for conservation laws) are used, which are TVD,and easy to extend to the multi-dimensions and converge fast. Secondly ENO(essentially nonoscillation ) method are used, which can be extended to higher order scheme and are not necessarilly TVD. The modified Roe scheme is used as a basic scheme for the both types of schemes. An aritificial compression method(ACM), improving resolution of the contact discontinuity, is applied for the both type of schemes, even though the ACM method was introduced for the ENO schemes. Two types of schemes are tested for the simple problems of the scalar wave, shock tube and the blast wave. More complicated problems are also solved for the steady flow around an arc bump and for the unsteady flow of moving schock in the presonce of a cylinder. It turns out the Minmod-ACM, which is in the first type is fast in convergence and reasonably accurate coparing with the ENO-ACM. Finally, a moving shock through a tube with abruptly varing area is calculated with the Minmod-ACM. Reflected waves after passing the larger area are propagated toward the inlet for the case of subsonic flow behind the shock, but the reflected waves are accumulated at the starting position of larger area for the case of supersonic flow behind the schock.

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서지기타정보
청구기호 {MAE 92002
형태사항 [iii], 41 p. : 삽화 ; 26 cm
언어 한국어
일반주기 저자명의 영문표기 : Duck-On Ko
지도교수의 한글표기 : 이덕주
지도교수의 영문표기 : Duck-Joo Lee
학위논문 학위논문(석사) - 한국과학기술원 : 항공우주공학과,
서지주기 참고문헌 : p. 20-21
주제 Lagrange equations.
Monotone operators.
Numerical analysis.
Euler 방정식. --과학기술용어시소러스
충격파. --과학기술용어시소러스
충격파관. --과학기술용어시소러스
변분법. --과학기술용어시소러스
Shock waves.
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