The international vortex flow experiment: A test case for compressible Euler codes

Report (1986)

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Copyright: Campus only
Supersonic flow Pressure distribution Transonic flow Vortices Compressible flow Wind tunnel tests Euler equations of motion Separated flow Delta wings International cooperation Leading edges Schlieren photography Navier Stokes equation Wingflow method test
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Published Date

31-10-1986

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NLR MP 86076 U

Abstract

As part of the joint International Vortex Flow Experiment, force and pressure measurements have been carried out on a 65 deg delta wing configuration in the transonic and supersonic wind tunnels of NLR. Out of these data three test cases were selected by the organizing committee of the GAMM WORKSHOP on the "Numerical Simulation of Compressible Euler Flows". The paper discusses these test cases in more detail, as well as other features of this type of flow. Paper presented at The GAMM-Workshop on the Numerical Simulation of Compressible Euler flows, INRIA; Rocquencourt, France, June 10-13, 1986.

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