Skip to main content
Log in

Zusammenfassung

Die Berechnung der Erwärmung stumpfer Flugkörper wird für grosse Geschwindigkeiten in Berücksichtigung der Übergangserscheinungen erörtert. Im besondern wird auf das Problem der Abkühlung durch Massentranspiration eingegangen.

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

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

References

  1. S. Goldstein,Modern Developments in Fluid Dynamics, 1st ed., vol. 2 (Oxford University Press, London 1938), p. 631.

    Google Scholar 

  2. M. Sibulkin,Heat Transfer Near the Forward Stagnation Point of a Body of Revolution, J. aeron. Sci.19, No. 8, 570–571 (August 1952).

    Google Scholar 

  3. I. Korobkin,Laminar Heat-Transfer Characteristics of a Hemisphere for Mach Number Range 1–9 to 4–9 (Heat Transfer and Fluid Mechanics Institute, June 23–25, 1955).

  4. H. A. Stine andK. Wanlass,Theoretical and Experimental Investigation of Aerodynamic-Heating and Isothermal Heat-Transfer Parameters on a Hemispherical Nose with Laminar Boundary Layer at Supersonic Mach Numbers, NACA TN 3344 (December 1954).

  5. E. R. van Driest,The Problem of Aerodynamic Heating, Aeron. Eng. Rev.15, No. 10, 26–41 (October 1956).

    Google Scholar 

  6. E. R. van Driest,On Turbulent Flow Near a Wall, J. aeron. Sci.23, No. 11, 1007–1011 (November 1956).

    MATH  Google Scholar 

  7. E. R. van Driest andJ. Christopher Boison,Research on Boundary-Layer Transition at Supersonic Speeds, J. aeron. Sci.24, No. 12, 885–899 (December 1957).

    Google Scholar 

  8. J. H. Clarke, H. R. Menkes andP. A. Libby,A Provisional Analysis of Turbulent Boundary Layers with Injection, J. aeron. Sci.22, No. 4, 255–260 (April 1957).

    Google Scholar 

  9. William H. Dorrance andFrank J. Dore,The Effect of Mass Transfer on the Compressible Turbulent Boundary-Layer Skin Friction and Heat Transfer, J. aeron. Sci.21, No. 6, 404–410 (June 1954).

    Google Scholar 

  10. Morris W. Rubesin,An Analytical Estimation of the Effect of Transpiration Cooling on the Heat-Transfer and Skin-Friction Characteristics of a Compressible, Turbulent Boundary Layer, NACA TN 3341 (December, 1954).

Download references

Author information

Authors and Affiliations

Authors

Additional information

This research was supported by the United States Air Force, through the Air Force Office of Scientific Research of the Air Research and Development Command, under contract AF 18(600)-786.

Rights and permissions

Reprints and permissions

About this article

Cite this article

van Driest, E.R. On the aerodynamic heating of blunt bodies. Journal of Applied Mathematics and Physics (ZAMP) 9, 233–248 (1958). https://doi.org/10.1007/BF02424748

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02424748

Keywords

Navigation