An investigation on supersonic bevelled nozzle jets

• المؤلفون الرئيسيون: Wu, Jie, New, Tze How
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2017
• الموضوعات: Supersonic jet; Shock cell structure
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/82308; http://hdl.handle.net/10220/43506
• المؤسسة: Nanyang Technological University

This paper reports upon a numerical and experimental study on supersonic jets exhausting from bevelled nozzles with 30° and 60° exit inclination angles. To begin with, a simple but effective method to design a shock-free convergent–divergent circular jet nozzle to produce a well-conditioned superson...