타이틀 |
Figure Control Simulations of Streamlined Adaptive-Walls |
저자 |
Masayoshi NAKAMURA, Asao HANZAWA |
Keyword |
Numerical flow simulation; Adaptive-wall control |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01284.pdf?id=NALTR0001284 |
보고서번호 |
NAL TR-1284 |
발행년도 |
1996.3 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
Bacause aerodynamic interferences between an airfoil model and wind-tunnel walls cannot be avoided in the structure of wind-t the inner flow match the outer flow at control surfaces.This requirement is satisfied by matching the pressure at two independent wall surfaces.Numerical wind-tunnel tests of NACA0012 and CAST10 airfoils were performed to demonstrate the potential applications of the adaptive-wall control.Several calculated results of airfoil abilities in the numerical wind tunnel are compared with experimental and with other calculated results. |