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IJSRP, Volume 9, Issue 4, April 2019 Edition [ISSN 2250-3153]

      Ujjwal Tiwari, Hao Tang, Anh Tu Dang

Abstract: 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.

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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:



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