Analysis of Supersonic Combustors with Swept Ramp Injectors

Author:

Baurle R. A.1,Alexopoulos G. A.1,Hassan H. A.1

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695-7910

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-08-25

2. DNS investigation on flame structure and scalar dissipation of a supersonic lifted hydrogen jet flame in heated coflow;International Journal of Hydrogen Energy;2013-08

3. Planar Imaging Investigation of Supersonic Hypermixer Configurations;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

4. Scalar and Velocity Measurements in a Mach 3 Hypermixing Flowfield;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

5. Simulations of Cavity-stabilized Flames in Supersonic Flows Using Reduced Chemical Kinetic Mechanisms;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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