Longo, J.M.A. and Radespiel, R. (1995) Numerical Simulation of Heat Transfer Effects on Two- Dimensional Steady Subsonic Flows. 26th AIAA Fluid Dynamics Conference 19-22 June, 1995.
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The aerodynamic characteristics of a flat plate and of a NACA airfoil with heated surface are presented in this paper. The flow field is simulated numerically by the solution of the Navier-Stokes equations. For the flat plate test case the flow is assumed steady, laminar and incompressible. The effects of grid coarsening on the solution, as well as the sensitivity of the flow field to variations of Reynolds number, Mach number, Prandtl number and surface temperature are shown. The numerical results compare well with the analytical solutions. For the NACA airfoil test case, the flow is assumed low compressible, turbulent and steady. The results indicate that maximum lift, maximum L/D and lift slope decrease with surface heating.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Numerical Simulation of Heat Transfer Effects on Two- Dimensional Steady Subsonic Flows|
|Keywords:||2D flows, boundary-layer flows, maximum lift, Navier-Stokes, numerical simulation, heat transfer effects, subsonic flows|
|Event Title:||26th AIAA Fluid Dynamics Conference 19-22 June, 1995|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 08:05|
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