THERMAL SCIENCE

International Scientific Journal

Authors of this Paper

External Links

AERODYNAMIC AND THERMAL ENVIRONMENT OF A GAP UNDER HYPERSONIC FLIGHT

ABSTRACT
Accurate prediction of aerodynamic and thermal environment around a gap has a significant effect on the development of spacecraft. The implicit finite volume schemes are derived and programmed from Navier-Stokes equations. Taking the gap between thermal insulation tiles as an example, a numerical simulation is performed by the finite volume method to obtain the flow characteristic in a gap and then to analyze the heat transfer mechanism. The numerical results are consistent with the experimental ones, which prove the precision of the method used in this paper. Furthermore, the numerical results reveal that the heat convection plays a leading role in heat transfer around a gap.
KEYWORDS
PAPER SUBMITTED: 2017-01-06
PAPER REVISED: 2017-06-20
PAPER ACCEPTED: 2017-09-01
PUBLISHED ONLINE: 2018-09-10
DOI REFERENCE: https://doi.org/10.2298/TSCI1804753H
CITATION EXPORT: view in browser or download as text file
THERMAL SCIENCE YEAR 2018, VOLUME 22, ISSUE Issue 4, PAGES [1753 - 1758]
REFERENCES
  1. Li, W. J., et al., A Coupled Thermal/Fluid/Chemical/Ablation Method on Surface Ablation of Charring Composites, International Journal of Heat and Mass Transfer, 109 (2017), Feb., pp. 725-736
  2. Li, W. J., et al., A Nonlinear Pyrolysis Layer Model for Analyzing Thermal Behavior of Charring Ablator, International Journal of Thermal Science, 98 (2015), Dec., pp. 104-112
  3. Huang, H. M., et al., Numerical Study on Aerodynamic Heat of Hypersonic Flight, Thermal Science, 20 (2016), 3, pp. 939 -944
  4. Li, W. J., et al., On the Novel Designs of Charring Composites for Thermal Protection Application in Reentry Vehicles, Applied Thermal Engineering, 93 (2016), Feb., pp. 849-855
  5. Li, W. J., et al., Protection of Pyrolysis Gases Combustion against Charring Materials' Surface Ablation, International Journal of Heat and Mass Transfer, 102 (2016), Jan., pp. 10-17
  6. Li, W. J., et al., A New Mechanism of Surface Ablation of Charring Materials for a Vehicle during Reentry, Applied Thermal Engineering, 106 (2016), Feb., pp. 838-849
  7. Nestler, D. E., et al., Heat Transfer to Steps and Cavities in Hypersonic Turbulent Flow, AIAA Journal, 7 (1969), 7, pp. 1368-1370
  8. Menter, F. R., Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications, AIAA Journal, 32 (1994), 8, pp. 1598-1605
  9. Avery, D. E., et al., Experimental Aerodynamic Heating to Simulated Shuttle Tiles, Journal of Spacecraft and Rockets, 22 (1985), 4, pp. 417-424
  10. Dunavant, J. C., et al., Aerodynamic Heat Transfer to RSI Tile Surfaces and Gap Intersections, Journal of Spacecraft and Rockets, 11 (1974), 6, pp. 437-440
  11. Gartimella, S., et al., Flow and Heat Transfer in Simulated Re-Entry Vehicle Tile Gaps, Journal of Thermophysics and Heat Transfer, 7 (1993), 4, pp. 644-650
  12. Turkel, E., Preconditioning Techniques in Computational Fluid Dynamics, Annual Review of Fluid Mechanics, 31 (1999), 1, pp. 385-416
  13. Turkel, E., Preconditioned Methods for Solving the Incompressible and Low Speed Compressible Equation, Journal of Computational Physics, 72 (1987), 2, pp. 277-298
  14. Weiss, J. M., et al., Implicit Solution of Preconditioned Navier-Stokes Equation Using Algebraic Multigrid, AIAA Journal, 37 (1999), 1, pp. 29-36
  15. Liou, M. S., A Sequel to AUSM, Part II: AUSM+-up for All Speeds, Journal of Computational Physics, 214 (2006), 1, pp. 137-170
  16. Qian, H. J. et al. Experimental Study on Heat Flux Distributions in Gaps, China Academy of Aerospace and Aerodynamics, Beijing, 1996

© 2024 Society of Thermal Engineers of Serbia. Published by the Vinča Institute of Nuclear Sciences, National Institute of the Republic of Serbia, Belgrade, Serbia. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution-NonCommercial-NoDerivs 4.0 International licence