Publication Date:
2006-06-13
Description:
Wind tunnel tests are performed in order to validate a computational fluid dynamics code. A large scale, two dimensional separation bubble is created on a flat plate, and low speed, turbulent flow is used. Extensive data sets are obtained with a nonintrusive laser velocimeter in addition to wall static pressure, total pressure, and hot-film measurements. All data and results are presented in a viewgraph format.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
NASA. Ames Research Center, NASA CFD Validation Workshop; p 616-648
Format:
text