Loading [MathJax]/jax/output/SVG/config.js
Prikladnaya Mekhanika i Tekhnicheskaya Fizika
RUS  ENG    JOURNALS   PEOPLE   ORGANISATIONS   CONFERENCES   SEMINARS   VIDEO LIBRARY   PACKAGE AMSBIB  
General information
Latest issue
Archive

Search papers
Search references

RSS
Latest issue
Current issues
Archive issues
What is RSS


Prikl. Mekh. Tekh. Fiz.:
Year:
Volume:
Issue:
Page:
Find




Personal entry:
Login:
Password:
Save password
Enter
Forgotten password?
Register

Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2010, Volume 51, Issue 1, Pages 22–28 (Mi pmtf1559)  
This article is cited in 3 scientific papers (total in 3 papers)

Bifurcations of transonic flow past simple airfoils with elliptic and wedge-shaped noses

A. G. Kuz'min

St. Petersburg State University, St. Petersburg, 198504, Russia
Full-text PDF (515 kB) Citations (3)
Abstract: A turbulent transonic flow past two symmetric airfoils with flat midparts is studied numerically. Using the Reynolds-averaged Navier–Stokes equations, we analyze the flow past a 9% thick airfoil with an elliptic nose. A range of the free-stream Mach number $\mathrm{M}_\infty$, in which flow bifurcations occur, is determined. Values of $\mathrm{M}_\infty$ that give rise to significant changes in the lift coefficient with variations of the angle of attack are specified. Flow bifurcations are also revealed for a thin double wedge, i.e., a sort of a hexagon.
Keywords: airfoil, local supersonic regions, buffet, bifurcations.
Received: 11.03.2009
English version:
Journal of Applied Mechanics and Technical Physics, 2010, Volume 51, Issue 1, Pages 16–21
DOI: https://doi.org/10.1007/s10808-010-0004-3
Bibliographic databases:
Document Type: Article
UDC: 533.6.011
Language: Russian
Citation: A. G. Kuz'min, “Bifurcations of transonic flow past simple airfoils with elliptic and wedge-shaped noses”, Prikl. Mekh. Tekh. Fiz., 51:1 (2010), 22–28; J. Appl. Mech. Tech. Phys., 51:1 (2010), 16–21
Citation in format AMSBIB
\Bibitem{Kuz10}
\by A.~G.~Kuz'min
\paper Bifurcations of transonic flow past simple airfoils with elliptic and wedge-shaped noses
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2010
\vol 51
\issue 1
\pages 22--28
\mathnet{http://mi.mathnet.ru/pmtf1559}
\elib{https://elibrary.ru/item.asp?id=13026103}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2010
\vol 51
\issue 1
\pages 16--21
\crossref{https://doi.org/10.1007/s10808-010-0004-3}
Linking options:
  • https://www.mathnet.ru/eng/pmtf1559
  • https://www.mathnet.ru/eng/pmtf/v51/i1/p22
    • This publication is cited in the following 3 articles:
    1. A. Kuzmin, “Instability of local supersonic regions over a flat-sided airfoil with a blunt trailing edge”, J. Phys.: Conf. Ser., 2103:1 (2021), 012208  crossref
    2. A. Kuzmin, “Transonic flow bifurcations over a double wedge”, J. Phys.: Conf. Ser., 1697:1 (2020), 012207  crossref
    3. Alexander Kuzmin, “Non-unique transonic flows over airfoils”, Computers & Fluids, 63 (2012), 1  crossref
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Prikladnaya Mekhanika i Tekhnicheskaya Fizika Prikladnaya Mekhanika i Tekhnicheskaya Fizika
    Statistics & downloads:
    Abstract page:55
    Full-text PDF :14
     
      Contact us:
    math-net2025_04@mi-ras.ru     		 Terms of Use  Registration to the website  Logotypes © Steklov Mathematical Institute RAS, 2025