Now showing items 1-5 of 5
Comparisons Between NO PLIF Imaging and CFD Simulations of Mixing Flowfields for High-Speed Fuel Injectors
(American Institute of Aeronautics and Astronautics, 2017)
Test-Model-Induced Interference Effects in Expansion Tube Flows
(American Institute of Aeronautics and Astronautics, 2016-01-02)
Enhanced Combustion in Supersonic Flows Using a Pulsed Detonation
(American Institute of Aeronautics and Astronautics, 2016-01-02)
Design and Characterization of the Michigan Hypersonic Expansion Tube Facility (MHExT)
(American Institute of Aeronautics and Astronautics, 2015-01-02)
Flow Characterization of a Hypersonic Expansion Tube Facility for Supersonic Combustion Studies
(American Institute of Aeronautics and Astronautics, 2017)