Open Access

ARTICLE

Effect of Sweptback Angle of a Delta Wing on Surface Pressure Distribution at Supersonic Mach Numbers

Shamitha Shetty^1,2, Asha Crasta¹, Sher Afghan Khan^3,*, Abdul Aabid⁴, Muneer Baig⁴

1 Mathematics Department, Mangalore Institute of Technology and Engineering, Visvesvaraya Technological University, Near Moodabidre, Mangaluru, Karnataka, 574225, India
2 Nitte Meenakshi Institute of Technology, Visvesvaraya Technological University, Bangalore, 560064, India
3 Department of Mechanical and Aerospace Engineering, Faculty of Engineering, International Islamic University Malaysia, Kuala Lumpur, 53100, Malaysia
4 Department of Engineering Management, College of Engineering Prince Sultan University, P.O. Box 66833, Riyadh, 11586, Saudi Arabia

* Corresponding Author: Sher Afghan Khan. Email: