05 - Propulsion and Energy
PARAMETRIC DESIGN AND MULTI-OBJECTIVE OPTIMIZATION OF EXHAUST NOZZLE FOR GAS TURBINE ENGINES
T.Q. Dinh¹, H.X. Vu¹, A.C. Pham¹, L.D. Chu¹; ¹Viettel Aerospace Institute, Vietnam
This study addresses the challenge of designing and optimizing a convergent exhaust nozzle for gas turbine engines, integrating CFD simulations with advanced sensitivity analysis and optimization techniques, to develop a systematic methodology for refining nozzle geometry to achieve superior flow characteristics.
DOI: 10.71945/icas2026_0579