Advertisement

Numerical Simulation of Laminar Hypersonic flow Past Blunt Bodies Including High Temperature Effects

  • G. Brenner
  • S. Riedelbauch
  • B. Müller
Part of the Notes on Numerical Fluid Mechanics (NNFM) book series (NNFM, volume 29)

Summary

Axisymmetric laminar hypersonic flows of perfect gas and equilibrium air past blunt bodies are simulated. The thin-layer Navier-Stokes equations are solved by a semi-implicit central finite-difference method. The thermodynamic and transport properties of equilibrium air are obtained from curve-fitting routines and from a Gibbs-energy minimization procedure. Results are obtained for a flow past a hemisphere and a hyperboloid.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. [1]
    Riedelbauch, S., Müller, B.: “The Simulation of Three-Dimensional Viscous Supersonic Flow Past Blunt Bodies with a Hybrid Implicit Explicit Finite-Difference Method”, DFVLR-FB 87-32 (1987).Google Scholar
  2. [2]
    Tannehill, J.C., Srinivasan, S., Weilmuenster, K.J.: “Simplified Curve Fits for the Thermodynamic Properties of Equilibrium Air”, NASA RP 1181 (1987).Google Scholar
  3. [3]
    Srinivasan, S., Tannehill, J.C., Weilmuenster, K.J.: “Simplified Curve Fits for the Transport Properties of Equilibrium Air”, Final Report, NASA CR 180422 (1987).Google Scholar
  4. [4]
    Bailey, H.E.: “Programs for computing equilibrium Thermodynamic properties of gases”, NASA TN D-3921, April 1967.Google Scholar
  5. [5]
    Peng, T., Pindroh, A.L.: “An Improved Calculation of Gas Properties at High Temperatures Air”, D-11722, The Boeing Company, 1962.Google Scholar
  6. [6]
    Hirschfelder, J., Curtis, C., Bird, B.: “Molecular Theory of Gases”, John Wiley & Sons, New York, 1954.zbMATHGoogle Scholar
  7. [7]
    Pfitzner, M., Weiland, C.: “3-D Euler Solution for Hypersonic Mach Numbers”, AGARD Conference Proceeding, AGARD-CP 428 (1987).Google Scholar
  8. [8]
    Brenner, G., Riedelbauch, S., Müller, B.: “The Computation of Axi-symmetric Hypersonic Air Flow in Chemical Equilibrium. Part I: The Use of Curve-Fitting Routines”, DLR-IB 221-89 A10, 1989.Google Scholar
  9. [9]
    Vigneron, Y.C.: “Hypersonic Flow of Equilibrium Air around Blunt Bodies”. Thesis, lowa State University, 1976.Google Scholar
  10. [10]
    Miller, III, C.G.: “Shock Shapes on Blunt Bodies in Hypersonic-Hypervelocity Helium, Air, and CO2 Flows, and Calibration Results in Langley 6-inch Expansion Tube”. NASA TN-D-7800, 1975.Google Scholar
  11. [11]
    Vincenti, W.G., Kruger, C.H.: “Introduction to Physical Gas Dynamic”. J. Wiley, New York, 1965.Google Scholar

Copyright information

© Springer Fachmedien Wiesbaden 1990

Authors and Affiliations

  • G. Brenner
    • 1
  • S. Riedelbauch
    • 1
  • B. Müller
    • 1
  1. 1.DLR Institute for Theoretical Fluid MechanicsGöttingenGermany

Personalised recommendations