Optimized semi-flexible supersonic nozzle design using exact throat solution with characteristic inversion and Bézier Mach distribution
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0274744
Authors: Honggang Qin, Qiang Peng, Xingyou Yi, Ning Wang, YunQiang Zhang
Institution: China Aerodynamics Research and Development Center
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4414853253