Skip to main content
SpringerLink
Log in

Supersonic aerodynamic characteristics of delta wings at high angles of attack

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

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

Access this article

Log in via an institution

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

Instant access to the full article PDF.

Institutional subscriptions

References

  1. A. P. Bazzhin, “Calculation of the flow past plane triangular wings at large angles of attack”, Izv. AN SSSR, MZhG [Fluid Dynamics], no. 5, 1966.

  2. M. P. Falunin and G. S. Ul'yanov, “Delta wing in supersonic flow (experimental results, M=3, γ=1.4)”, Izv. AN SSSR, MZhG [Fluid Dynamics], no. 6, 1967.

  3. C. H. Melellan, M. N. Bertram, and J. A. Morre, “An investigation of four wings of square planform at Mach number of 6.9 in the Langley 11-inch hypersonic tunnel”, NACA, Rep., no. 1310, 1957.

Download references

Author information

Authors and Affiliations

  1. Moscow

    M. P. Falunin, G. S. Ul'yanov, A. A. Makshin & A. F. Mosin

Authors
  1. M. P. Falunin
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. G. S. Ul'yanov
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. A. A. Makshin
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. A. F. Mosin
    View author publications

    You can also search for this author in PubMed Google Scholar

Rights and permissions

Reprints and permissions

About this article

Cite this article

Falunin, M.P., Ul'yanov, G.S., Makshin, A.A. et al. Supersonic aerodynamic characteristics of delta wings at high angles of attack. Fluid Dyn 3, 105–108 (1968). https://doi.org/10.1007/BF01029549

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01029549

Keywords

Search

Navigation