Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Program Management and Integration Department, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology
We develop the new wall interference correction method for the 2 m x 2 m transonic speed wind tunnel in the JAXA Wind Tunnel Technology Center. In this method we describe a wind tunnel, model and support system and lift effect by the sink and source panels and the doublets. And the restriction parameter R is introduced as the perforated wall boundary condition. We can get the wall interference from the strength of sinks and souses on the wind tunnel panels, which satisfy the boundary conditions. In the report we show how to get the R and the R value of the perforated cart of the JAXA transonic speed wind tunnel.
JAXA2m×2m遷音速風洞壁境界修正用境界条件の設定
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