All Issue

2024 Vol.29, Issue 4 Preview Page

Original Article

31 December 2024. pp. 10-23
Abstract
References
1

2005, Lips, T. and Fritsche, B., "A Comparison of Commonly Used Re-entry Analysis Tools," Acta Astronaut., Vol.57, No.2-8, pp.312-323.

10.1016/j.actaastro.2005.03.010
2

2008, Kim, C.W., Lee, Y.G. and Lee, D.S., "Aerodynamic Analysis of Sub-orbital Re-entry Vehicle," J. Comput. Fluids Eng., Vol.13, No.2, pp.1-7.

3

2020, Viviani, A., Aprovitola, A., Iuspa, L. and Pezzela, G., "Aeroshape Design of Reusable Re-entry Vehicles by Multidisciplinary Optimization and Computational Fluid Dynamics," Aerosp. Sci. Technol., Vol.105, 106029.

10.1016/j.ast.2020.106029
4

2014, Colombo, C., Letizia, F., Alessi, E.M. and Landgraf M., "End-of-life Earth Re-entry for Highly Elliptical Orbits : The Integral Mission," The 24th AAS/AIAA Space Flight Mechanics Meeting.

5

2010, Savino, R., Paterna, D., Fumo D.S. and D'Elia, M., "Plasma-Radiofrequency Interactions Around Atmospheric Re-Entry Vehicles : Modelling and Arc-Jet Simulation," The Open Aerospace Engineering Journal, Vol.3, pp.76-85.

10.2174/1874146001003010076
6

2020, Chae, J.H., Mankodi, T.K., Choi, S.M. and Myong, R.S., "Combined Effects of Thermal Non-equilibrium and Chemical Reactions on Hypersonic Air Flows Around An Orbital Reentry Vehicle," Int. J. Aeronaut. Space Sci., Vol.21, pp.612-626.

10.1007/s42405-019-00243-9
7

2020, Ejtehadi, O. and Myong, R.S., "A Modal Discontinuous Galerkin Method for Simulating Dusty and Granular Gas Flows in Thermal Non-equilibrium in the Eulerian Framework," J. Comput. Phys., pp.1-43.

8

2020, Mankodi, T.K., Bhandarkar, U.V. and Myong, R.S., "Collision Corss Sections and Nonequilibrium Viscosity Coefficients of N2 and O2 based on Molecular Dynamics," Phys. Fluids, Vol.32, 036102.

10.1063/1.5141148
9

2019, Mankodi, T.K. and Myong, R.S., "Quasi-classical Trajectory-based Non-equilibrium Chemical Reaction Models for Hypersonic Air Flows," Phys. Fluids, Vol.31, 106102.

10.1063/1.5119147
10

2023, Won, B., Park, Y., Han, N., Lee, E. and Shin, E., "A Study on Characteristics of Needle-Punching C/C in High-Enthalpy Plasma and High-Velocity Flame Environments," J. Korean Soc. Aeronaut. Space Sci., Vol.51, No.4, pp.235-242.

10.5139/JKSAS.2023.51.4.235
11

1998, Lee, M.G., "Aerodynamic Heating Prediction of Reacting Blunt Body Flow with an Impinging Shock Wave," International Heat Transfer Conference, Vol.4, pp.207-212.

10.1615/IHTC11.3690PMC124835
12

2003, Liever, P.A., Habchi, S.D., Burnell, S.I. and Lingard, J.S., "Computational Fluid Dynamics Predistion of the Beagle 2 Aerodynamic Database," J. Spacecr. Rockets, Vol.40, No.5, pp.632-638.

10.2514/2.6911
13

2012, Pezzella, G. and Trifoni, E., "Aerothermodynamic Design of an Ablative Heat Shield Design for a Sample Return Vehicle," 4th Sino-Italian Conference on Space Aerothermodynamics and Hot Structures, pp.52-64.

14

2001, Desai, P.N. and Cheatwood, F.M., "Entry Dispersion Analysis for the Genesis Sample Return Capsule," J. Spacecr. Rockets, Vol.38, No.3, pp.345-350.

10.2514/2.3707
15

2019, Mankodi, T.K. and Myong, R.S., "Investigation of Non-Equilibrium Reacting Air Flow Around Stardust Re-entry Vehicle," J. Korean Soc. Aeronaut. Space Sci., pp.20-21.

16

2014, Kang, E.J., Kim, J.Y., Park, J.H. and Myong, R.S., "Computational Investigation of the High Temperature Reacting Gas Effects on Re-entry Vehicle Flowfields," J. Comput. Fluids Eng., Vol.19, No.1, pp.7-14.

10.6112/kscfe.2014.19.1.007
17

2003, Lee, C.H. and Park, S.O., "Effects of Nose Radius of Blunt Body on Aerodynamic Heating in Thermochemical Nonequilibrium Flow," J. Comput. Fluids Eng., Vol.8, No.4, pp.34-40.

18

2019, Chae, J.H., Lee, J.W. and Myong, R.S., "Computational Thermal Analysis of Earth Reentry Vehicles for Different Flight Missions," J. Comput. Fluids Eng., Vol.2019, No.10, pp.34.

19

2017, Mehta, R.C., "Effect of Geometrical Parameters of Reentry Capusle over Flowfield at High Speed Flow," Adv. Aircr. Spacecr. Sci., Vol.4, No.4, pp.487-501.

20

2000, Komurasaki, K. and Candler, G.V., "Laminar-to-Turbulent Transitions over an Ablating Reentry Capsule," Acta Astronaut., Vol.47, No.10, pp.745-751.

10.1016/S0094-5765(00)00117-X
21

2012, Shiva, P.U. and Srinivas, G., "Flow Simulation over Re-Entry Bodies at Supersonic & Hypersonic Speeds," Int. J. Eng. Res. Dev., Vol.2, No.4, pp.29-34.

22

2014, Kang, E.J., Kim, J.Y., Chun, S.H., Myong R.S. and Cho T.H., "Investigation of the Stability and Controllability of a Re-entry Vehicle Using Compuational Aerodynamic Analysis," J. Comput. Fluids Eng., Vol.2012, No.5, pp.247-250.

23

2018, Fadgyas, M.C., Pricop, M.V., Niculescu, M.L., Cojocaru, M.G. and Dumitrache, A., "Semi-Empirical Relations for Pressure Distributions in Hypersonic Regime," International Conference of Numerical Analysis and Applied Mathematics 2017, 370007.

10.1063/1.5043975
24

2021, Michna, J., Rogowski, K., Bangga, G. and Hansen, M.O.L., "Accuracy of the Gamma Re-Theta Transition Model for Simulating the DU-91-W2-250 Airfoil at High Reynolds Numbers," Energies, Vol.14, No.24, p.8224.

10.3390/en14248224
25

2020, Aliaga, C., Guan, K., Selvanayagam, J., Stokes, J., Viti, V. and Menter F., "Hypersonic Applications of the Laminar-Turbulent Transition SST Model in ANSYS Fluent," AIAA Aviation 2020 Forum, p.3290.

10.2514/6.2020-3290
26

1959, Hansen, C.F., "Approximations for the Thermodynamic and Transport Properties of High-temperature Air," NASA Technical Note 4150.

27

2007, Paolo, B., Sylvian G., Patrice, P. and Jacques M., "Pre-X Atmospheric Re-entry Experimental Lifting Body: Program Status and System Synthesis," Acta Astronaut., Vol.61, pp.459-474.

10.1016/j.actaastro.2007.01.053
28

2004, Kim, H.D., Matsuo, S. and Setoguchi, T., "Passive Control Applied to Prandtl-Meyer Expansion Flow with Homogeneous Condensation," Aerosp. Sci. Technol., Vol.8, pp.369-376.

10.1016/j.ast.2004.02.002
29

2020, Mehta, R.C., "Computation of Base Pressure Based on to Fill-up the Growing Space Applied to Reentry Capsules," AIAA Aviation 2020 Forum.

10.2514/6.2020-2711
30

2009, Hirschel, E.H. and Weiland C., Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, American Institute of Aeronautics and Astronautics, Springer, pp.357-369.

Information
  • Publisher :Korean Society for Computational Fluids Engineering
  • Publisher(Ko) :한국전산유체공학회
  • Journal Title :Journal of Computational Fluids Engineering
  • Journal Title(Ko) :한국전산유체공학회지
  • Volume : 29
  • No :4
  • Pages :10-23
  • Received Date : 2024-06-01
  • Revised Date : 2024-08-12
  • Accepted Date : 2024-12-09