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Investigation in the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles.

机译：对高超音速/低超音速战术导弹使用固体燃料冲压发动机的可行性的研究。

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http://archive.org/details/investigationinf00witt

机译：HTTP://archive.org/details/investigation inf00Witt

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作者
Witt Michael A.;
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年度 1989
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原文格式 PDF
正文语种 en_US
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3. Experimental and numerical investigation on the ignition and combustion stability in solid fuel ramjet with swirling flow [J] . Musa Omer, Chen Xiong, Zhou Changsheng Acta astronautica . 2017,第auga期

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5. Investigation of Laser Discharge in a Supersonic Flow and Shock Wave Laminar Boundary Layer Interaction in a Hypersonic Flow [D] . Mortazavi Ravari, Mahsaalsadat. 2018

机译：超音速流中激光放电与高音速流中冲击波层流边界层相互作用的研究
6. Experimental investigation on the characteristics of supersonic fuel spray and configurations of induced shock waves [O] . Yong Wang, Yu-song Yu, Guo-xiu Li, -1

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7. Design and testing of a caseless solid-fuel integral-rocket ramjet engine for use in small tactical missiles. [O] . Fruge Keith J. 1991

机译：用于小型战术导弹的无壳固体燃料整体火箭冲压发动机的设计和测试。

Investigation in the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles.

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