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Hypersonic aircraft and inlet configurations derived from axisymmetric flowfields

Hypersonic aircraft and inlet configurations derived from axisymmetric flowfields

Hamdi T. Hemdan
  • 作者Hamdi T. Hemdan
  • 卷第21卷
  • 期第9期
  • 印刷ISSN0094-5765
  • 文件大小545.26KB
  • 发表时间1990
  • DOI10.1016/0094-5765(90)90072-s
  • 页码609-616
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