Scramjet engines: The first forty years

被引:461
作者
Curran, ET [1 ]
机构
[1] USAF, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
D O I
10.2514/2.5875
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A general review of the emergence and maturing of supersonic combustion ramjet (scramjet) engine technologies over the last 40 years is presented. The review is given in terms of the efforts completed or proceeding in the United States, Russia, France, Germany, Japan, Australia, and other countries. A brief account of the challenges of scramjet combustor development is given, and attention is directed toward other source references for more detailed accounts of technology evolution. Two emerging scramjet applications are identified, namely, hydrogen-fueled high-speed engines for access to space and hydrocarbon-fueled engines for hypersonic air-launched missiles.
引用
收藏
页码:1138 / 1148
页数:11
相关论文
共 104 条
  • [1] ALBEGOV RV, 1991, FIZ GOREN VZRYVA, V27, P24
  • [2] Andrews E. H., 1994, 107759 NASA TM
  • [3] Andrews E.H., 1993, AIAA Paper 93-2323
  • [4] [Anonymous], X2895 NASA TM
  • [5] [Anonymous], 925094 AIAA
  • [6] BAKOS RJ, 1999, P 14 INT S AIR BREAT
  • [7] Billig F. S., 1972, P 1 INT S AIR BREATH
  • [8] Billig F.S., 1993, AIAA Paper 93-2329
  • [9] BILLIG FS, 1972, J SPACECRAFT ROCKETS, V9, P702
  • [10] COMBUSTION PROCESSES IN SUPERSONIC-FLOW
    BILLIG, FS
    [J]. JOURNAL OF PROPULSION AND POWER, 1988, 4 (03) : 209 - 216