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Aissaoui Mohammed Islem

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Open access Jul 2026

Effect of Straight and Compound Blade Lean on the Aerodynamic Performance of a High-Pressure Turbine Nozzle Guide Vane under Residual Swirl

The exhaust flow at the outlet of modern lean-burn combustors, which offer reduced NOx emissions for gas turbines, is characterized by hot streaks (HS) and residual swirl that affect the aerothermal performance of downstream high-pressure (HP) turbine nozzle guide vanes (NGVs). Although leaned blades are widely employe...

Aissaoui Mohammed Islem, Salaheddine Azzouz, Z. Mansouri · 0 citations

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