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ArticleJ-GLOBAL ID:200902018978069531整理番号:90A0098247

Comparison of theory and experiment for four supercritical, low drag airfoils.

四つのスーパークリティカル,低抗力翼形に対する理論と実験の比較

著者:JONES D J(National Research Council, Ottawa, CAN)、KHALID M(National Research Council, Ottawa, CAN)、EGGLESTON B(deHavilland Aircraft, Ontario, CAN)
資料名:AGARD Conf Proc 号:437 Vol.2 ページ:P8.1-P8.16
発行年:1988年12月
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