关注
Taimur Ali Shams
Taimur Ali Shams
在 cae.nust.edu.pk 的电子邮件经过验证
标题
引用次数
引用次数
年份
Failure analysis of a broken support strut of an aircraft landing gear
A Hameed, O Zubair, TA Shams, Z Mehmood, A Javed
Engineering Failure Analysis 117, 104847, 2020
252020
Airfoil selection procedure, wind tunnel experimentation and implementation of 6dof modeling on a flying wing micro aerial vehicle
TA Shams, SIA Shah, A Javed, SHR Hamdani
Micromachines 11 (6), 553, 2020
252020
Estimation of stability parameters for wide body aircraft using computational techniques
M Ahmad, ZL Hussain, SIA Shah, TA Shams
Applied Sciences 11 (5), 2087, 2021
212021
Techniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review
S Afridi, TA Khan, SIA Shah, TA Shams, K Mohiuddin, DJ Kukulka
Energies 16 (15), 5721, 2023
132023
Vertical take-off and landing hybrid unmanned aerial vehicles: An overview
M Rehan, F Akram, A Shahzad, TA Shams, Q Ali
The Aeronautical Journal 126 (1306), 2017-2057, 2022
132022
Comprehensive design of an oleo-pneumatic nose landing gear strut
MA Ahmad, SIA Shah, TA Shams, A Javed, STI Rizvi
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2021
112021
Experimental investigation of propeller induced flow on flying wing micro aerial vehicle for improved 6DOF modeling
TA Shams, SIA Shah, A Shahzad, A Javed, K Mehmod
IEEE Access 8, 179626-179647, 2020
112020
Numerical analysis of bladeless ceiling fan: An effective alternative to conventional ceiling fan
K Mehmood, A Shahzad, J Masud, F Akram, MN Mumtaz, TA Shams
Journal of Wind Engineering and Industrial Aerodynamics 221, 104905, 2022
92022
Study of Low Reynolds Number Aerodynamics for Low Aspect Ratio MAV Wing
TA Shams, SIA Shah, MA Ahmad
2018 IEEE 21st International Multi-Topic Conference (INMIC), 1-8, 2018
72018
Numerical Investigation on the Thrust Vectoring Performance of Bypass Dual Throat Nozzle
S Afridi, TA Khan, SIA Shah, TA Shams, K Mehmood, W Li, D Kukulka
Energies 16 (2), 594, 2023
62023
Design space optimisation of an unmanned aerial vehicle submerged inlet through the formulation of a data-fusion-based hybrid model
F Akram, HA Khan, TA Shams, D Mavris
The Aeronautical Journal 125 (1292), 1815-1832, 2021
62021
Capability analysis of global hypersonic wind tunnel facilities for aerothermodynamic investigations
TA Shams, SIA Shah, MA Ahmad
2020 17th International Bhurban Conference on Applied Sciences and …, 2020
52020
A stabilized RBF finite difference method for convection dominated flows over meshfree nodes
A Javed, F Mazhar, TA Shams, M Ayaz, N Hussain
Engineering Analysis with Boundary Elements 107, 159-167, 2019
52019
Selection methodology of composite material for retractable main landing gear strut of a lightweight aircraft
MA Ahmad, H Rafiq, SIA Shah, SA Khan, STI Rizvi, TA Shams
Applied Sciences 12 (11), 5689, 2022
42022
Design optimization of bladeless ceiling fan using design of experiments
K Mehmood, A Shahzad, F Akram, TA Shams, MN Mumtaz, J Masud
Journal of Wind Engineering and Industrial Aerodynamics 233, 105313, 2023
32023
Selection methodology of an electric actuator for nose landing gear of a light weight aircraft
TA Shams, SIA Shah, MA Ahmad, K Mehmood, W Ahmad, STI Rizvi
Applied Sciences 10 (23), 8730, 2020
32020
Steady Analysis of NACA Flush Inlet at High Subsonic and Supersonic Speeds
JM Taimur Ali Shams
Proceedings of the World Congress on Engineering 2015 2, 1261-1266, 2015
3*2015
Evaluating the side force in oseen flow slender body theory and comparison with CFD simulation results
HM Khan, TA Shams, E Chadwick
Proceedings of the World Congress on Engineering 3, 2115-2119, 2013
32013
A Novel Framework for Qualification of a Composite-Based Main Landing Gear Strut of a Lightweight Aircraft
MA Ahmad, SI Ali Shah, SA Khan, HA Khan, TA Shams
Polymers 15 (6), 1402, 2023
22023
Aerodynamic analysis of hummingbird-like hovering flight
N Haider, A Shahzad, MNM Qadri, TA Shams
Bioinspiration & Biomimetics 16 (6), 066018, 2021
22021
系统目前无法执行此操作,请稍后再试。
文章 1–20