Skip to main content

Attached High-Speed Viscous Flow

  • Chapter
Book cover Basics of Aerothermodynamics
  • 1876 Accesses

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 149.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 189.00
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

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. E. H. Hirschel. “Evaluation of Results of Boundary-Layer Calculations with Regard to Design Aerodynamics”. AGARD R-741, 1986, pp. 5-1 to 5-29.

    Google Scholar 

  2. J. Cousteix, D. Arnal, B. Aupoix, J. Ph. Brazier, A. Lafon. “Shock Layers and Boundary Layers in Hypersonic Flows”. Progress in Aerospace Sciences, Pergamon Press, Vol. 30, 1994, pp. 95–212.

    Article  Google Scholar 

  3. E. H. Hirschel. “Vortex Flows: Some General Properties, and Modelling, Configurational and Manipulation Aspects”. AIAA-Paper 96-2514, 1996.

    Google Scholar 

  4. E. H. Hirschel, W. Kordulla. “Shear Flow in Surface-Oriented Coordinates”. Notes on Numerical Fluid Mechanics, Vol. 4. Vieweg, Braunschweig/Wiesbaden, 1981.

    Google Scholar 

  5. D. C. Wilcox. “Turbulence Modelling for CFD”. DCW Industries, La Cañada, CAL., USA, 1998.

    Google Scholar 

  6. R. B. Bird, W. E. Stewart, E. N. Lightfoot. “Transport Phenomena”. John Wiley, New York and London/Sydney, 2nd edition, 2002.

    Google Scholar 

  7. L. Prandtl. “Über Flüssigkeitsbewegung bei sehr kleiner Reibung”. Proc. Third International Mathematical Congress, Heidelberg, Germany, 1904.

    Google Scholar 

  8. D. Frederick, T. S. Chang. “Continuum Mechanics”. Allyn and Bacon, Boston, Mass., 1965.

    Google Scholar 

  9. D. R. Chapman, M. W. Rubesin. “Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature”. Journal of the Aeronautical Sciences, Vol. 16, 1949, pp. 547–565.

    MathSciNet  Google Scholar 

  10. E. H. Hirschel. “Boundary-Layer Coordinates on General Wings and Fuselages”. Zeitschrift für Flugwissenschaften und Weltraumforschung (ZFW), Vol. 6, No. 3, 1982, pp. 194–202.

    Google Scholar 

  11. M. van Dyke. “Perturbation Methods in Fluid Mechanics”. The Parabolic Press, Stanford, 1975.

    Google Scholar 

  12. B. Aupoix, J. Ph. Brazier, J. Cousteix, F. Monnoyer. “Second-Order Effects in Hypersonic Boundary Layers”. J. J. Bertin, J. Periaux, J. Ballmann (eds.), Advances in Hypersonics, Vol. 3, Computing Hypersonic Flows. Birkhäuser, Boston, 1992, pp. 21–61.

    Google Scholar 

  13. R. Courant, D. Hilbert. “Methods of Mathematical Physics”. Vol. II. John Wiley-Interscience, New York, 1962.

    Google Scholar 

  14. M. W. Rubesin, H. A. Johnson. “A Critical Review of Skin Friction and Heat Transfer Solutions of the Laminar Boundary Layer of a Flat Plate”. Trans. ASME, Vol. 71, 1949, pp. 385–388.

    MathSciNet  Google Scholar 

  15. E. R. G. Eckert. “Engineering Relations of Friction and Heat Transfer to Surfaces in High-Velocity Flow”. J. Aeronautical Sciences, Vol. 22, No. 8, 1955, pp. 585–587.

    MATH  Google Scholar 

  16. G. Simeonides, L. Walpot, M. Netterfield, G. Tumino. “Evaluation of Engineering Heat Transfer Prediction Methods in High Enthalpy Flow Conditions”. AIAA-Paper 96-1860, 1996.

    Google Scholar 

  17. E. H. Hirschel. “Untersuchung grenzschichtähnlicher Strömungen mit Druckgradienten bei grossen Anström-Machzahlen (Investigation of Boundary Layer Like Flows at Large Free-Stream Mach Numbers)”. Inaugural Thesis, RWTH Aachen, Germany, 1975, also DLR FB 76-22, 1976.

    Google Scholar 

  18. Y. C. Vigneron, J. V. Rakich, J. C. Tannehill. “Calculation of Supersonic Viscous Flows over Delta Wings with Sharp Subsonic Leading Edges”. AIAAPaper 78-1137, 1978.

    Google Scholar 

  19. E. H. Hirschel. “Untersuchungen zum Problem Normaler Druckgradienten in Hyperschallgrenzschichten”. Laminare und turbulente Grenzschichten. DLR Mitt. 71-13, 1971, pp. 51–73.

    Google Scholar 

  20. H. Schlichting. “Boundary Layer Theory”. 7th edition, McGraw-Hill, New York, 1979.

    Google Scholar 

  21. F. M. White. “Viscous Fluid Flow”. McGraw-Hill, New York, 2nd edition, 1991.

    Google Scholar 

  22. E. R. G. Eckert, R. M. Drake. “Heat and Mass Transfer”. MacGraw-Hill, New York, 1950.

    Google Scholar 

  23. G. Simeonides. “On the Scaling of Wall Temperature Viscous Effects”. ESA/ESTEC EWP-1880, 1996.

    Google Scholar 

  24. M. J. Lighthill. “On Displacement Thickness”. J. Fluid Mechanics, Vol. 4, 1958, pp. 383–392.

    Article  MATH  MathSciNet  Google Scholar 

  25. F. Monnoyer, Ch. Mundt, M. Pfitzner. “Calculation of the Hypersonic Viscous Flow past Reentry Vehicles with an Euler-Boundary Layer Coupling Method”. AIAA-Paper 90-0417, 1990.

    Google Scholar 

  26. G. Simeonides. “Hypersonic Shock Wave Boundary Layer Interactions over Compression Corners”. Doctoral Thesis, University of Bristol, U.K., 1992.

    Google Scholar 

  27. G. B. Schubauer, P. S. Klebanoff. “Contributions on the Mechanics of Boundary Layer Transition”. NACA TN 3489, 1955, and NACA R 1289, 1956.

    Google Scholar 

  28. W. Mangler. “Zusammenhang zwischen ebenen und rotatiossymmetrischen Grenzschichten in kompressiblen Flüssigkeiten”. ZAMM, Vol. 28, 1948, pp. 97–103.

    MATH  MathSciNet  Google Scholar 

  29. E. Reshotko. “Heat Transfer to a General Three-Dimensional Stagnation Point”. Jet Propulsion, Vol. 28, 1958, pp. 58–60.

    Google Scholar 

  30. E. Reshotko, I. E. Beckwith. “Compressible Laminar Boundary Layer over a Yawed Infinite Cylinder with Heat Transfer and Arbitrary Prandtl Number”. NACA R 1379, 1958.

    Google Scholar 

  31. G. Simeonides. “Generalized Reference-Enthalpy Formulation and Simulation of Viscous Effects in Hypersonic Flow”. Shock Waves, Vol. 8, No. 3, 1998, pp. 161–172.

    Article  MATH  Google Scholar 

  32. L. Lees. “Laminar Heat Transfer over Blunt-Nosed Bodies at Hypersonic Speeds”. Jet Propulsion, Vol. 26, 1956, pp. 259–269.

    Google Scholar 

  33. J. D. Anderson. “Hypersonic and High Temperature Gas Dynamics”. McGraw-Hill, New York, 1989.

    Google Scholar 

  34. G. Simeonides. “Simple Formulations for Convective Heat Transfer Prediction over Generic Aerodynamic Configurations and Scaling of Radiation-Equilibrium Wall Temperature”. ESA/ESTEC EWP 1860, 1995.

    Google Scholar 

  35. J. A. Fay, F. R. Riddell. “Theory of Stagnation Point Heat Transfer in Dissociated Gas”. Journal of Aeronautical Science, Vol. 25, No. 2, 1958, pp. 73–85.

    MathSciNet  Google Scholar 

  36. D. I. A. Poll. “Transition Description and Prediction in Three-Dimensional Flow”. AGARD-R-709, 1984, pp. 5-1 to 5-23.

    Google Scholar 

  37. E. H. Hirschel. “Thermal Surface Effects in Aerothermodynamics”. Proc. Third European Symposium on Aerothermodynamics for Space Vehicles, Noordwijk, The Netherlands, November 24–26, 1998. ESA SP-426, 1999, pp. 17–31.

    Google Scholar 

  38. M. A. Schmatz, R. K. Höld, F. Monnoyer, Ch. Mundt, H. Rieger, K. M. Wanie. “Numerical Methods for Aerodynamic Design II”. Space Course 1991, RWTH Aachen, 1991, pp. 62-1 to 62-40.

    Google Scholar 

  39. R. Radespiel. Personal communication. 1994.

    Google Scholar 

  40. I. Oye, H. Norstrud. “Personal communication”. 2003.

    Google Scholar 

  41. W. Schröder, R. Behr, S. Menne. “Analysis of Hypersonic Flows Around Space Transportation Systems via CFD Methods”. AIAA-Paper 93-5067, 1993.

    Google Scholar 

Download references

Rights and permissions

Reprints and permissions

Copyright information

© 2005 Springer Berlin Heidelberg

About this chapter

Cite this chapter

(2005). Attached High-Speed Viscous Flow. In: Basics of Aerothermodynamics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-26519-8_7

Download citation

  • DOI: https://doi.org/10.1007/3-540-26519-8_7

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-22132-6

  • Online ISBN: 978-3-540-26519-1

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics