NASA NTRS · 20180003622
Combustor Assembly for a Turbine Engine
Abstract
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel injectors. The bulkhead forms a combustion chamber with the first and the second walls. The fuel injectors are configured with the first wall in a unique and/or a fluctuating pattern.
Keep this discovery
Explore connections, maps & timelines
Dai, Zhongtao, Cohen, Jeffrey M., Kopp-Vaughan, Kristin, Hoke, James B.. 2018-05-01. Combustor Assembly for a Turbine Engine. https://ntrs.nasa.gov/citations/20180003622
Cite the original work for its findings. Save a collection to share your selection of sources.