MUSHTAQ, NORAIZ
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Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines
2025-01-01 Mushtaq, N.; Pini, M.; Gaetani, P.
ADVANCED DESIGN OF A TRANSITION DUCT FOR SUPERSONIC INLET TURBINES IN ROTATING DETONATION ENGINES
2024-01-01 Mushtaq, N.; Pini, M.; Gaetani, P.
Design and Parametric Analysis of a Supersonic Turbine for Rotating Detonation Engine Applications
2022-01-01 Mushtaq, N.; Colella, G.; Gaetani, P.
Development of a Reduced Order Model for Turbine Blade Cooling Design
2025-01-01 Pinardi, Andrea; Mushtaq, Noraiz; Gaetani, Paolo
Large eddy simulation of a supersonic inlet turbine in a rotating detonation engine
2025-01-01 Mushtaq, N.; Arroyo, C. P.; Dombard, J.; Duchaine, F.; Strempfl, P.; Gaetani, P.
THE EFFECT OF UPSTREAM UNSTEADINESS ON THE UNSTARTING OF A SUPERSONIC INLET TURBINE
2023-01-01 Mushtaq, N.; Gaetani, P.
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine
2024-01-01 Mushtaq, N.; Gaetani, P.
The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines
2023-01-01 Mushtaq, N; Persico, G; Gaetani, P
THE ROLE OF ENDWALL SHAPE OPTIMIZATION IN THE DESIGN OF SUPERSONIC TURBINES FOR ROTATING DETONATION ENGINES
2022-01-01 Mushtaq, N.; Persico, G.; Gaetani, P.
Understanding and modeling unstarting phenomena in a supersonic inlet cascade
2023-01-01 Mushtaq, N.; Gaetani, P.
UNSTARTING PHENOMENA IN THE DESIGN OF A SUPERSONIC INLET TURBINE
2023-01-01 Mushtaq, N.; Gaetani, P.