• NATO Research and Technology Organization Working Group on Technologies for Propelled Hypersonic Flight

• Continued Inlet-Isolator Model Development and Application to H ₂ and HC Fueled Dual-Mode Scramjet Test Data

• Continued Development of the VULCAN CFD Code

Past Projects

• Hyper-X

• JP-7 Endothermic Fuel Heater for Direct Connect Supersonic Combustion Test Facility
  
  
• USAF/P&W GDE-2 Test in 8-FT HT

• ISTAR RBCC Ground Demonstration Engine

  • Government Lead for RBCC Scramjet Flowpath Development
  • Injector Characterization Rig (ICR) tests with heated JP-7 in the DCSCTF
  • VULCAN FNS of RBCC Dual-Mode Scramjet Flowpath and Comparison with Test Data
  • Smale-Scale Inlet Tests in the M4BDF and VULCAN FNS CFD
  • High Speed Cascade Injector
    • Cold Flow Mixing and Hot Flow Combustion Tests
    • VULCAN FNS of Limited SHIP DOE Cases, Cold Flow Mixing and Combustion Tests
  • Low Speed/Transonic Generic Configuration Aero-Propulsive Tests

 

 

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