Publication Date:
2019-07-13
Description:
This paper describes a series of wind tunnel experiments carried out with the aim of providing data suitable for evaluating the performance of Computational Fluid Dynamics (CFD) codes. The configurations and flow conditions studied are most relevant to slender supersonic missiles. However, the data obtained, which includes forces and moments, surface pressures, flowfield surveys and a selection of flow visualization images, should he of interest to other CFD practitioners. Results for three test cases are presented and discussed in this paper. These cases have been the subject of a collaborative study concerned with the evaluation of Navier-Stokes solvers for missiles, carried out under the auspices of The Technical Cooperation Programme (TTCP).
Keywords:
Fluid Mechanics and Thermodynamics
Type:
AIAA Paper 2000-4207
,
Applied Aerodynamics; Aug 14, 2000 - Aug 17, 2000; Denver, CO; United States
Format:
text
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