극초음속 유동장 재돌입체에 대한 공력 계산 Aerodynamics Calculation of Reentry Body in Hypersonic Flowfield
한국기계기술학회지
(韓國機械技術學會誌)
제15권 제6호
(2013.12)
pp.819-825
pp.819-825
한국기계기술학회
(Korean Society of Mechanical Technology)
초록
Aerodynamic coefficients of a reentry bodyin hypersonic flowfiled are calculated by using a three-dimensional flow solver. The high temperature real gas effects, thermal excitations and chemical reactions of air, are accounted for in the calculation. The reasonable agreement between the calculated aerodynamic coefficients and the Apollo AS-202 flight date are obtained. The effects of thermochemical nonequilibrium on the aerodynamic predictions are shown to be non-negligible.
목차
Abstract
1. Introduction
2. Method of calculations
2.1 Governing Equations
2.2 Thermochemical models
2.3 Transport properties
2.4 Numerical methods
3. Test Conditions
4. Results and Discussions
5. Summary
Acknowledgements
References
1. Introduction
2. Method of calculations
2.1 Governing Equations
2.2 Thermochemical models
2.3 Transport properties
2.4 Numerical methods
3. Test Conditions
4. Results and Discussions
5. Summary
Acknowledgements
References
저자