1. Parametric study on the drag and heat flux reduction mechanism of forward-facing cavity on a blunt body in supersonic flows;Huang;Aerosp. Sci. Technol.,2017
2. Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles;Huang;Aerosp. Sci. Technol.,2015
3. Computational fluid dynamics study of optimized hypersonic leading edge geometries;Hinman,2015
4. Parametric geometry models for hypersonic aircraft components: blunt leading edges;Kontogiannis,2015
5. Optimization of Bezier curves for high speed leading edge geometries;Rodi,2013