Finite element least square method for solving full steady Euler equations in a plane nozzle

  • C. H. Bruneau
  • J. J. Chattot
  • J. Laminie
  • J. Guiu-Roux
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 170)


A finite element least square method is applied to the steady Euler equations in a nozzle or a channel. For the capture of shock waves an artificial density formula is used. Fast convergence is achieved with I.C.C.G. algorithm.


Shock Wave Mach Number Transonic Flow Exit Pressure Convergent Divergent Nozzle 
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Copyright information

© Springer-Verlag 1982

Authors and Affiliations

  • C. H. Bruneau
    • 1
    • 2
  • J. J. Chattot
    • 3
  • J. Laminie
    • 4
  • J. Guiu-Roux
    • 1
  1. 1.Université de Paris-SudOrsayFrance
  2. 2.Office National d'Etudes et de Recherches Aérospatiales (O.N.E.R.A.)ChâtillonFrance
  3. 3.MATRAVelizyFrance
  4. 4.C.N.R.S. E.R.A. 297OrsayFrance

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