All Issue

2025 Vol.30, Issue 1 Preview Page

Original Article

31 March 2025. pp. 39-50
Abstract
References
1

2024, Acket-Goemaere, A., Brukardt, R., Klempner, J., Sierra, A. and Stokes, B., "Space: The $1.8 trillion opportunity for global economic growth," McKinsey's Aerospace & Defense Practice, World Economic Forum, Inisght Report.

2

2024, Kulakhmetov, M.F., Alviani, R., Rao, A., Murray, V., Taylor, J.B., Seik, J. and Vaughan, E., "Optimizing Optical Emission Measurements on the Varda Hypersonic Testbed Vehicle," AIAA Aviation Forum and Ascend, p.4560.

3

2009, Hirschel, E.H. and Weiland, C., "Selected aerothermodynamic design problems of hypersonic flight vehicles," Springer Science & Business Media, Vol.229.

4

2009, Theisinger, J.E. and Braun, R.D., "Multi-objective hypersonic entry aeroshell shape optimization," J. Spacecr. Rockets, Vol.46, No.5, pp.957-966.

10.2514/1.41136
5

2010, Nosratollahi, M., Mortazavi, M., Adami, A. and Hosseini, M., "Multidisciplinary design optimization of a reentry vehicle using genetic algorithm," Aircr. Eng. Aerosp. Technol., Vol.82, No.3, pp.194-203.

10.1108/00022661011075928
6

2011, Cavallero, C., Chiarelli, C., Mareschi, V., Davite, A., Gallizio, F., Minisci, E. and Sudars, M., "Multi- disciplinary shape optimization of an entry capsule integrated with custom neural network approximation and multi-fidelity approach," Eurogen 2011 Conference.

7

2014, Dirkx, D. and Mooij, E., "Optimization of entry-vehicle shapes during conceptual design," Acta Astronaut. Vol.94, No.1, pp.198-214.

10.1016/j.actaastro.2013.08.006
8

2022, Kabganian, M., Hashemi, S.M. and Roshanian, J., "Multidisciplinary Design Optimization of a Re-Entry Spacecraft via Radau Pseudospectral Method," Appl. Mech., Vol.3, No.4, pp.1176-1189.

10.3390/applmech3040067
9

2024, Yeo, H., Lee, M., Kim, D. and Kim, K.H., "Multi-objective Optimization Design Framework and Flight Performance Prediction for Reentry Module Using a Rapid Analysis Program," Int. J. Aeronaut. Space Sci., pp.1-13.

10

2010, Kontinos, D.A. and Wright, M.J., "Introduction: Atmospheric entry of the stardust sample return capsule," J. Spacecr. Rockets, Vol.47, No.6, pp.865-867.

10.2514/1.52887
11

2006, Anderson, J.D., "Hypersonic and high temperature gas dynamics," AIAA.

12

1995, Sharma, R.K., Theerthamalai, P. and Panneerselvam, S., "Aerodynamic characteristics of forebody-cylinder combinations of circular/non-circular cross section at angles of attack", Twelfth Australasian Fluid Mechanics Conference, University of Sydney, Australia, pp. 695-698.

13

2005, Meador, W.E. and Smart, M.K., "Reference enthalpy method developed from solutions of the boundary-layer equations," AIAA J., Vol.43, No.1, pp.135-139.

10.2514/1.2656
14

2021, Lee, M., Lee, J., Kim, K.H. and Kim, H., "Efficient aerodynamic analysis of air-breathing hypersonic vehicle using local surface inclination method based on unstructured meshes," Int. J. Aeronaut. Space Sci., Vol.22, No.5, pp.1031-1041.

10.1007/s42405-021-00370-2
15

1999, Mitcheltree, R.A., Wilmoth, R.G., Cheatwood, F.M., Brauckmann, G.J. and Greene, F.A., "Aerodynamics of Stardust sample return capsule," J. Spacecr. Rockets, Vol.36, No.3, pp.429-435.

10.2514/2.3463
16

2010, Trumble, K.A., Cozmuta, I., Sepka, S., Jenniskens, P. and Winter, M., "Postflight aerothermal analysis of the stardust sample return capsule," J. Spacecr. Rockets, Vol.47, No.5, pp.765-774.

10.2514/1.41514
17

2009, Kinney, D., "Development of the ORION crew exploration vehicle's aerothermal database using a combination of high fidelity CFD and engineering level methods," 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, p. 1100.

18

2014, Brandis, A.M. and Johnston, C.O., "Characterization of stagnation-point heat flux for earth entry," 45th AIAA Plasmadynamics and Lasers Conference, p. 2374.

19

2013, Mazaheri, A., Gnoffo, P.A., Johnston, C.O. and Kleb, W.L., "LAURA Users Manual: 5.5-65135," NASA TM-2013-217800

20

2008, Johnston, C.O., Hollis, B.R. and Sutton, K., "Spectrum modeling for air shock-layer radiation at lunar-return conditions," J. Spacecr. Rockets, Vol.45, No.5, pp.865-878.

10.2514/1.33004
21

2008, Johnston, C.O., Hollis, B.R. and Sutton, K., "Non-Boltzmann modeling for air shock-layer radiation at lunar-return conditions," J. Spacecr. Rockets, Vol.45, No.5, pp.879-890.

10.2514/1.33006
22

2009, Steinfeldt, B., Theisinger, J., Korzun, A., Clark, I., Grant, M. and Braun, R., "High mass mars entry, descent, and landing architecture assessment," AIAA Space 2009 Conference & Exposition, p. 6684.

10.2514/6.2009-6684
23

2015, Sepka, S. and Samareh, J.A., "Thermal protection system mass estimating relationships for blunt-body, earth entry spacecraft," 45th AIAA Thermophysics Conference, p. 2507.

24

2011, Thornton, J., Ghandehari, E.M., Fan, W., Stackpoole, M. and Chavez-Garcia, J., "PICA variants with improved mechanical properties. In National Space and Missile Materials Symposium," No. ARC-E-DAA-TN3674.

25

2012, Fortin, F.A., De Rainville, F.M., Gardner, M.A.G., Parizeau, M. and Gagne, C., "DEAP: Evolutionary algorithms made easy," J. Mach. Learn. Res., Vol.13, No.1, pp.2171-2175.

Information
  • Publisher :Korean Society for Computational Fluids Engineering
  • Publisher(Ko) :한국전산유체공학회
  • Journal Title :Journal of Computational Fluids Engineering
  • Journal Title(Ko) :한국전산유체공학회지
  • Volume : 30
  • No :1
  • Pages :39-50
  • Received Date : 2024-12-05
  • Revised Date : 2025-02-04
  • Accepted Date : 2025-02-04