T11-95 Blunt Fin Interaction
(Japan)

Updated on 08/31/95


Brief Description

The test is proposed to assess codes simulating 3D supersonic shock-wave / boundary-layer turbulent interaction on an unswept fin/plate configuration with a blunt leading edge.

Focal Point


Full Description


Working Group Chairman

Shigeru Aso
Kyushu University
Department of Aeronautics and Astronautics
6-10-1 Hakozaki, Higashi-ku, Fukuoka 812, Japan
(tel) +81-92-6411101 ext. 5789 or 5790
(fax) +81-92-6515863
e-mail: aso@aero.kyushu-u.ac.jp

Date of last change: August 31, 1995
hsff@math.uh.edu