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Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63

机译：在马赫数为0.4到4.63的两级和三级火箭配置的1/7比例模型的俯仰中的空气动力学特性

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Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63

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作者
Fournier, R. H.; Hinson, W. F.; Langhans, R. A.;
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年度 1969
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC COEFFICIENTS; ROCKET VEHICLES; SCALE MODELS; STAGE SEPARATION; MACH NUMBER; PITCHING MOMENTS; RESEARCH VEHICLES; SOLID ROCKET PROPELLANTS;

机译：空气动力学系数;火箭车辆;尺度模型;阶段分离;马赫数; pITCHING mOmENTs;研究车辆;固体火箭推进剂;

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8. Aerodynamic Characteristics in Pitch of a 1/7-Scale Model of a Two- and Three-Stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 [R] . Fournier, R. H., Hinson, W. F., Langhans, R. A. 1969

机译：在马赫数为0.4到4.63的两级和三级火箭构型的1/7比例模型的俯仰中的气动特性

Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63

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