26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-2.2.1

COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA

M. Murayama, Y. Yokokawa, H. Kato, K. Masahiro, K. Yamamoto, T. Ito
JAXA, Japan

Keywords: High-Lift, CFD

In JAXA, a research program to develop design technologies for advanced high-lift devices has been conducted combining CFD and wind tunnel testing. A series of tests using an aircraft high-lift model have been conducted from 2005 to 2008. In this paper, computational studies related to the tests are presented.

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