NASA Common Research Model 80％縮尺模型遷音速風洞詳細試験データの取得及び公開

Aeronautical and Space Sciences Japan

Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663

Acquisition and Publication of Transonic Wind Tunnel Test Data of the 80% Scaled NASA Common Research Model

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2019 Volume 67 Issue 1 Pages 2

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