DESIGN-MODEL OF HIGH-PERFORMANCE RAMJET OR SCRAMJET-POWERED VEHICLES

被引：1
|
作者：
SCHINDEL, LH
机构：
[1] Naval Surface Warfare Center, Silver Spring, MD
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1990年 / 27卷 / 06期
关键词：
D O I：
10.2514/3.26188
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A procedure is described for designing a long-range, high-speed vehicle integrating airframe and propulsion components. As envisioned here, the process involves the following steps: 1) establish performance criteria, 2) vary engine and airframe parameters to optimize performance, and 3) find a configuration that fits these desired parameters. In this paper, an approximate analysis of scramjet or ramjet engine performance is developed and coupled with appropriate airframe parameters. An example is provided to show how the procedure could be applied to the preliminary design of a scramjet-powered missile that cruises at March number 6.
引用
收藏
页码：613 / 617
页数：5
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