Skip to main content
Log in

Subsonic and transonic flow field in two-dimensional de laval nozzles

  • Published:
Acta Mechanica Sinica Aims and scope Submit manuscript

Abstract

This paper presents solutions of subsonic and transonic flow fields in two-dimensional De Laval nozzles with preassinged contraction ration 1, expansion ration 2, and throat wall radiusR *. The effects of the contraction and the expansion angle on nozzle flow, the transformation of flow pattern of a De Laval nozzle in the throat region, and the conditions of occurrence and the governing parameters of the supersonic bubbles are discussed.

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.

Institutional subscriptions

Similar content being viewed by others

References

  1. Lin, T.C. and Jia Zhenxue, Proc. Indian Acad. Sic. (Engg. Sci.),4, 3 (1981), 315–345.

    Google Scholar 

  2. Lin, T.C. and Jia Zhenxue,Acta Mechanica Sinica,1 (1978), 1–18.

    MATH  Google Scholar 

  3. Venillot, J.P. and Viriand, H.,AI AA J.,17, 7 (1970), 691–692.

    Google Scholar 

  4. Ishii, R.,Phys. Fluids,21, 4 (1978), 540–548.

    Article  MATH  MathSciNet  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Qun, P., Tongji, L. Subsonic and transonic flow field in two-dimensional de laval nozzles. Acta Mech Sinica 1, 1–8 (1985). https://doi.org/10.1007/BF02487855

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02487855

Key Words

Navigation