An Investigation of the Aerodynamic Stabilizing Effectiveness of Several Split Flare Afterbody Configurations in the Presence of an Underexpanded Jet Plume at Transonic Mach Numbers.

著录项

• 作者

  burt,james r.;

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• 作者单位

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• 年度 1978
• 页码 1-83
• 总页数 83
• 原文格式 PDF
• 正文语种 eng
• 中图分类 工业技术;
• 关键词

  Guided missiles; Aerodynamic stability; Flared afterbodies; Boundary layer flow; Tube launched; Folding fins(Rockets); Exhaust plumes; Thrust control; Wind tunnel tests; Splitting; Transonic flight; Mach number; Angle of attack;

  机译：导弹;气动稳定性;扩张后体;边界层流;管发射;折叠鳍（火箭）;排气羽;推力控制;风洞试验;分裂;跨音速飞行;马赫数;攻角;