Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow

• المؤلفون الرئيسيون: Crasta, Asha, Pavithra, S, Khan, Sher Afghan
• التنسيق: مقال
• اللغة: English; English
• منشور في: NOVA Science Publishers 2016
• الموضوعات: T175 Industrial research. Research and development
• الوصول للمادة أونلاين: http://irep.iium.edu.my/53341/1/paper2.pdf; http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf; http://irep.iium.edu.my/53341/; http://www.novapublishers.com

In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence ang...