Fluid Phenomena in Scramjet Combustion Systems

• E T Curran ^[1] ; W H Heiser ^[2] ; D T Pratt ^[3]
  1. [1] Wright-Patterson Air Force Base

     Wright-Patterson Air Force Base

     Township of Bath, Estados Unidos

     
  2. [2] United States Air Force Academy

     United States Air Force Academy

     Estados Unidos

     
  3. [3] University of Washington

     University of Washington

     Estados Unidos

     

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• Localización: Annual review of fluid mechanics, ISSN 0066-4189, Nº. 28, 1996, págs. 323-360
• Idioma: inglés
• Texto completo no disponible (Saber más ...)
• Resumen

  • This paper reviews important advances in understanding and predicting the behavior of scramjet combustion systems since the classic article published in this series by Antonio Fed (1973). The review focuses on basic fluid phenomena and is divided into three distinct sections. The first briefly describes progress that has been made in the design and demonstration of practical scramjets around the world, especially in the US, the FSU, France, and Germany. The second provides a contemporary exposition of the aerothermodynamics of the dual-mode ramjetkcramjet combustion system, accounting for the role of the isolator in preventing unstart from either thermal choking or flow separation due to heat release. The third part summarizes the current state of knowledge regarding fuel- air mixing in dual-mode ramjetkcramjet combustors, especially the potential of axial vorticity to increase mixing effectiveness over that of lateral vorticity.