Process development for grid generations to simulate hypersonic flow around a generic re-entry capsule

• المؤلف الرئيسي: Krishna Contractor
• مؤلفون آخرون: Jorg Uwe Schluter
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2016
• الموضوعات: DRNTU::Engineering::Aeronautical engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/68796

After the retirement of the Space shuttle, space agencies around the world have turned to space return capsules for re-entry missions. During re-entry into the atmosphere, the capsule undergoes manoeuvres at extremely high speeds reaching 20 Mach and beyond. At such hypersonic conditions, several...