| Comparison of flow-solvers: Linear vortex lattice method and higher-order panel method with analytical and wind tunnel data T Shahid, F Sajjad, M Ahsan, S Farhan, S Salamat, M Abbas 2020 3rd International Conference on Computing, Mathematics and Engineering …, 2020 | 8 | 2020 |
| Applicability of 3D printed fighter aircraft model for subsonic wind tunnel A Raza, S Farhan, S Nasir, S Salamat 2021 International Bhurban Conference on Applied Sciences and Technologies …, 2021 | 6 | 2021 |
| Faqir M Abbas, S Farhan M, A, 1689-1699, 0 | 4 | |
| Optimal Wave Drag Reduction Technique for Fighter Aircraft Using von Kármán Ogive and Haack Series H Jamal, SMF Naveed, MZ Javed, M Ahsan, S Salamat Pakistan Journal of Engineering and Technology 4 (1), 151-158, 2021 | | 2021 |
Muneeb AhsanDept of Aerospace Engg, Air University, PAC Kamra, Pakistan在 aerospace.pk 的电子邮件经过验证
Muneeb AhsanDept of Aerospace Engg, Air University, PAC Kamra, Pakistan在 aerospace.pk 的电子邮件经过验证