Flow calculation over a delta-wing using the thin-layer wavier-stokes equations

Kumar, Anand (1989) Flow calculation over a delta-wing using the thin-layer wavier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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Abstract

A 3D laminar thin-layer Navier-Stokes solver is developed13; which employs finite volume spatial discretisation and13; Runge-Kutta time integration. The code is applied to compute vortex flow over a round leading edge delta wing, and the results are compared with experiment and an Euler simulation.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Navier-stokes equatins;Vortex flow
Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
Depositing User: Users 64 not found.
Date Deposited: 31 Jul 2006
Last Modified: 24 May 2010 04:14
URI: http://nal-ir.nal.res.in/id/eprint/1950

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