Convergent-Divergent Nozzle Design

I need a skilled engineer to design a Convergent-Divergent supersonic nozzle for jet aircraft propulsion.

Requirements

- Design should optimize performance for aerospace propulsion applications. - Must consider factors like pressure ratios, temperature, and flow characteristics. - Provide detailed drawings and specifications. Ideal Skills and Experience: - Background in aerospace engineering. - Experience with nozzle design, particularly for jet aircraft. - Proficiency in CAD software. - Strong understanding of fluid dynamics and thermodynamics.