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Filtering by: Creator Zelina, Joseph Creator Erdmann, Timothy J., jr.

Experimental Studies of Cavity and Core Flow Interactions With Application to Ultra-Compact Combustors

Creator:

Blunck, David L., Shouse, Dale T., Neuroth, Craig, Lynch, Amy, Erdmann, Timothy J., Jr., Burrus, David L., Zelina, Joseph, Richardson, Daniel, and Caswell, Andrew

Abstract:

Reducing the weight and decreasing pressure losses of aviation gas turbine engines improves the thrust-to-weight ratio and improves efficiency. In ultra-compact combustors (UCC), engine length is reduced and pressure losses are decreased by merging a combustor with adjacent components using a systems engineering approach. High-pressure turbine inlet vanes can be...

Resource Type:

Article

Full Text:

Innovative Scientific Solutions Inc., Dayton, OH 45459 e-mail: david.burrus.1.ctr@us.af.mil Joseph Zelina