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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.15 Number.1
- 발행연도
- 2014.3
- 수록면
- 91 - 96 (6page)
이용수
초록· 키워드
오류제보하기
The aim of this work is to determine supersonic nozzle profiles that are used in propulsion, for launchers or embarked with satellites. This design has the role of firstly, providing important propulsion, i.e. with uniform and parallel flow at exit; and secondly, to find short length profiles, without modification of the flow in the nozzle. The first elaborate program is used to determine the profile of the divergent, by using the characteristics method for an axisymmetric flow. The second program is conceived by using the finite volume method, to determine and test the profile found connected to a convergent.
목차
Abstract
1. Introduction
2. Mathematic Formulation
3. Calculation And Programming
4. Results And Interpretation
5. Conclusion
References
참고문헌 (6)
참고문헌 신청
1. [단행본] - Shapiro, A.H. / 1954 / The Dynamics and Thermodynamics of Compressible fluid flow / The Ronald Press Company
2. [학술대회논문] - Van Leer, B. / 1982 / Flux Vector Splitting for the Euler Equations / Lecture Notes in Physics, Eighth International Conference on Numerical Methods in Fluid Dynamics 170 : 507 ~ 512
3. [학술지(정기간행물)] - Haoui, R. / 2001 / Chemical and vibrational nonequilibrium flow in a hypersonic axisymmetric nozzle / International Journal of Thermal Sciences 40 (8) : 787 ~ 795
4. [학술지(정기간행물)] - Haoui, R. / 2010 / Finite volumes analysis of a supersonic non-equilibrium flow around the axisymmetric blunt body / International Journal of Aeronautical and space Sciences 11 (2) : 59 ~ 68
5. [학술대회논문] - Haoui, R. / 2003 / Condition of convergence applied to an axisymmetric reactive flow / French Congress of Mechanics
2. [학술대회논문] - Van Leer, B. / 1982 / Flux Vector Splitting for the Euler Equations / Lecture Notes in Physics, Eighth International Conference on Numerical Methods in Fluid Dynamics 170 : 507 ~ 512
3. [학술지(정기간행물)] - Haoui, R. / 2001 / Chemical and vibrational nonequilibrium flow in a hypersonic axisymmetric nozzle / International Journal of Thermal Sciences 40 (8) : 787 ~ 795
4. [학술지(정기간행물)] - Haoui, R. / 2010 / Finite volumes analysis of a supersonic non-equilibrium flow around the axisymmetric blunt body / International Journal of Aeronautical and space Sciences 11 (2) : 59 ~ 68
5. [학술대회논문] - Haoui, R. / 2003 / Condition of convergence applied to an axisymmetric reactive flow / French Congress of Mechanics
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UCI(KEPA) : I410-ECN-0101-2015-550-001318218