Ultra-Compact combustion presents an innovative solution to address the demand for increasingly compact, efficient, and low weight aircraft gas turbine engine propulsion systems. An Ultra-Compact Combustor (UCC) operates by diverting a portion of the compressor exit flow into a cavity about the engine outer diameter. Injection into the cavity can be done at an angle to induce bulk circumferential swirl.
Ujjwal Tiwari, Hao Tang, Anh Tu Dang (2019); Numerical Investigation of Influence of Cavity Air Injection Panels in Ultra-Compact Combustor; International Journal of Scientific and Research Publications (IJSRP)
9(4) (ISSN: 2250-3153), DOI: http://dx.doi.org/10.29322/IJSRP.9.04.2019.p8897