Propulsion: Hypersonic Propulsion Systems: Design, Dual-Mode Combustion and Systems Off-Design Simulation: Combustion Stability of a Dual-Mode Scramjet - Configuration with Strut Injector

Sara Rocci-Denis, Armin Brandstetter, Dieter Rist, Hans Peter Kau

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Original languageEnglish
Title of host publicationBasic Research and Technologies for Two-Stage-to-Orbit Vehicles
PublisherJohn Wiley and Sons
Number of pages19
ISBN (Print)3527277358, 9783527277353
StatePublished - 7 Nov 2005


  • Airbreathing propulsion systems
  • Dual-mode combustion
  • Gasdynamically optimized fuel injectors
  • Hypersonic inlets
  • Hypersonic propulsion systems
  • Lobed strut injectors
  • Nozzle flow fields
  • PDF/FDF-methods
  • Propulsion
  • Research
  • Supersonic and hypersonic transport
  • Supersonic combustion
  • Supersonic flames
  • Supersonic turbulent combustion
  • Systems off-design simulation
  • Technologies for two-stage-to-orbit vehicles
  • Viscous interaction effects

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