Pressure distributions on a flat-plate delta wing swept 65 deg at a Mach number of 5.97 at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at a 90 deg angle of attack

著录项

• 作者

  Goldberg, T. J.; Hondros, J. G.;

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• 作者单位

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• 年度 1962
• 页码 1-28
• 总页数 28
• 原文格式 PDF
• 正文语种 eng
• 中图分类 工业技术;
• 关键词

  ANGLE OF ATTACK; DELTA WINGS; FLAT PLATES; HYPERSONIC SPEED; MACH NUMBER; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; ROLL; SWEPT WINGS; ANGLE OF ATTACK; DELTA WING; FLAT PLATE; HYPERSONIC SPEED; PRESSURE DISTRIBUTION; SWEPT WING;

  机译：攻击角度; DELTa WINGs;平板;超速的;马赫数;压力分布; REYNOLDs NUmBER;滚; sWEpT WINGs;攻击角度; DELTa WING;平板;超速的;压力分布; sWEpT WING;