Skip to main content

Application of Finite Difference TVD Methods in Hypersonic Aerodynamics

  • Conference paper
  • First Online:
Finite Difference Methods,Theory and Applications (FDM 2014)

Part of the book series: Lecture Notes in Computer Science ((LNTCS,volume 9045))

Included in the following conference series:

Abstract

The numerical method for solving of the hypersonic nonequilibrium aerogasdynamics problems is suggested. The method is based on the full three-dimensional Navier-Stokes equations, supplemented by the equations of chemical kinetics and the finite difference TVD method. The developed algorithms are implemented in the computer-aided software package SIGMA. The results of simulation of the hypersonic flow about the spherical nose segment of a model hypersonic vehicle are presented.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 39.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Harten, A.: High resolution schemes for hyperbolic conservation laws. J. Comp. Phys. 49, 357–393 (1983)

    Article  MATH  MathSciNet  Google Scholar 

  2. Gil’manov, A.N.: Metody adaptivnyx setok v zadachax gazovoj dinamiki [Methods of Adaptive Meshes in Gas Dynamic Problems]. Fizmatlit, Moscow (2000)

    Google Scholar 

  3. Anderson, J.D.: Hypersonic and High-Temperature Gas Dynamics, 2nd edn. American Institute of Aeronautics and Astronautics, Reston (2006)

    Book  Google Scholar 

  4. Dimitrienko, Y.I., Kotenev, V.P., Zakharov, A.A.: Metod lentochnyh adaptivnyh setok dlja chislennogo modelirovanija v gazovoj dinamike [Methods of Adaptive Band-Net Meshes for Numerical Simulation in Gas Dynamics]. Fizmatlit, Moscow (2011)

    Google Scholar 

  5. Dimitrienko, Y.I., Zakharov, A.A., Koryakov, M.N.: Razrabotka programmnogo obespechenija dlja chislennogo modelirovanija v zadachah giperzvukovoj ajerogazodinamiki perspektivnyh letatel’nyh apparatov [Software development for numeral modeling of hypersonic aerogasdynamics problem perspective aircrafts]. Programmnye sistemy: teorija i prilozhenija: jelektron. nauchn. zhurn. 3(4), 17–26 (2012). http://psta.psiras.ru/read/psta2012_4_17-26.pdf

    Google Scholar 

  6. Hirschfelder, J.O., Curtiss, C.F., Bird, R.B.: Molecular Theory of Gases and Liquids. American Institute of Aeronautics and Astronautics, Wiley, New York (1954)

    MATH  Google Scholar 

Download references

Acknowledgements

The reported study was supported by the Supercomputing Center of Lomonosov Moscow State University.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Yury Dimitrienko .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2015 Springer International Publishing Switzerland

About this paper

Cite this paper

Dimitrienko, Y., Koryakov, M., Zakharov, A. (2015). Application of Finite Difference TVD Methods in Hypersonic Aerodynamics. In: Dimov, I., Faragó, I., Vulkov, L. (eds) Finite Difference Methods,Theory and Applications. FDM 2014. Lecture Notes in Computer Science(), vol 9045. Springer, Cham. https://doi.org/10.1007/978-3-319-20239-6_15

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-20239-6_15

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-20238-9

  • Online ISBN: 978-3-319-20239-6

  • eBook Packages: Computer ScienceComputer Science (R0)

Publish with us

Policies and ethics