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EXPERIMENTAL INVESTIGATION OF BLAST LOADING ON AN AIRFOIL IN MACH NUMBER 0.7 AIRFLOW WITH INITIAL ANGLE-OF-ATTACK CHANGE OF 20 DEG

机译：机载0.7气流中翼型爆破加载实验研究初始角度为20°的初始角度变化

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Blast loading on airfoil in high subsonic airflow - diffraction

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作者
Manning, J. C.; Pierce, H. B.;
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年度 1963
页码 1-38
总页数 38
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIR FLOW; AIRFOILS; ANGLE OF ATTACK; BLAST LOADS; DIFFRACTION; LOW SPEED; SUBSONIC FLOW; SUBSONIC SPEED; TELEMETRY; AIRFOIL; BLAST LOADING; DIFFRACTION; SUBSONIC FLOW;

机译：空气流动;翼型;攻击角度;爆炸负荷;衍射;低速; sUBsONIC FLOW; sUBsONIC spEED;遥测;翼型;爆破装载;衍射; sUBsONIC FLOW;

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8. Experimental Investigation of Blast Loading on an Airfoil in Mach 0.7 Airflow with Initial Angle-of-Attack Change of 28 Deg [R] . Manning, J. C. 1965

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EXPERIMENTAL INVESTIGATION OF BLAST LOADING ON AN AIRFOIL IN MACH NUMBER 0.7 AIRFLOW WITH INITIAL ANGLE-OF-ATTACK CHANGE OF 20 DEG

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