Numerical Simulation of Unsteady Vortical Flow about Delta Wings Oscillating at High Incidence

Author:

Fritz W.

Publisher

Vieweg+Teubner Verlag

Reference11 articles.

1. Wagner B., Hitzel S. M., Schmatz M. A., Schwarz W., Hilgenstock. A., Scherr S.: Status of CFD validation on the VORTEX FLOW Experiment. AGARD CP-437 (1988) Vol. 1., pp. 10–1 to 10-10.

2. Longo J. M. A.: Verification des Rechenverfahrens CEVCATS für die Berechnung von Wirbelströmungen um Deltaflügel. In: ZfW 20/1996, Springer-Verlag, pp 213-226, 1996.

3. van den Berg J. L, Brandsma F. J.: Navier-Stokes Results for a Sharp Edged Delta Wing. Contribution of NLR to Phase VI of IEPG Panel III, SG6-TA 15. NLR Report NLR CR 94592 C, 1994.

4. Hummel, D.: Documentation of Separated Flows for Computational Fluid Dynamics Validation. In: AGARD Conference Proceedings No. 437, 1988.

5. Jameson A.: Time-Dependent Calculations Using Multigrid, with Applications to Unsteady Flows past Airfoils and Wings. AIAA Paper 91-1596, 1991.

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1. CFD simulations of a delta wing in high-alpha pitch oscillations;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

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