Project Title: CFD ANALYSIS OF CD NOZZLE AND EFFECTS ON PRESSUREAND VELOCITY FOR SUDDENLY EXPANDED FLOWS | Ansys Simulation.
Location: Fluid Mechanics Lab, HITEC University
Course Instructors:
M. Ammar Akram (Lecturer MED)
M. Hammad Asghar (Lab Engineer)
Students contributed:
Muhammad Ubaid Khalid
Muhammad Fakhar Tariq
Muhammad Bilal Sikandar
Syed Mohammad Assad Abdullah Hashmi
Kashaf Irshad
Abstract: In sudden expansion the effectiveness of jet plays a vital role in various application. Compressible flow regions in nozzles are dominated by intense pressure gradients and complex secondary flows. The work outlined in this paper is to design a supersonic convergentdivergent (CD) Nozzle. From the current analysis, it is clear that the maximum rise or decrease in pressure and velocity will occur for a particular Mach number and NPR effect.