The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration

Rumsey, Christopher L

关键词: BODY-WING CONFIGURATIONS;    TRAILING EDGES;    COMPUTATIONAL FLUID DYNAMICS;    WIND TUNNEL TESTS;    NASA PROGRAMS;   

RP-ID  :  NF1676L-28138

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separation and progression, was designed from the outset to be a highly collaborative effort between CFD computationalists and experimentalists. This paper highlights key aspects of the planning and execution of the project, which has recently completed its first phase of wind tunnel testing. The joint CFD/experimental team is described, and its accomplishments to date are summarized.