Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Abdul Munem Khan"'
Autor:
Muhammad Umer Sohail, Hossein Raza Hamdani, Asad Islam, Khalid Parvez, Abdul Munem Khan, Usman Allauddin, Muhammad Khurram, Hassan Elahi
Publikováno v:
Applied Sciences, Vol 11, Iss 8, p 3706 (2021)
Non-uniform inlet flows frequently occur in aircrafts and result in chronological distortions of total temperature and total pressure at the engine inlet. Distorted inlet flow operation of the axial compressor deteriorates aerodynamic performance, wh
Externí odkaz:
https://doaj.org/article/27122bb91f254db0ab661c7f13fc8890
Publikováno v:
NUST Journal of Engineering Sciences, Vol 2, Iss 1 (2009)
Applying numerical optimization techniques, a propeller of conventional geometry is designed from composite materials. Ply orientation angles of the composite material have been used as the design variables, to achieve various design objectives. The
Externí odkaz:
https://doaj.org/article/b4cd74f5bd064242aa5d9793d5bd212a
Publikováno v:
Journal of Energy Resources Technology. :1-23
With the ever increasing demand of energy necessitates the utilization of renewable energy sources such as wind energy. Wind turbines are widely used to convert wind energy into electrical and mechanical energy, with constant improvement in design so
Autor:
Hassan Elahi, Muhammad Khurram, Usman Allauddin, Asad Islam, Khalid Parvez, Hossein Raza Hamdani, Abdul Munem Khan, Muhammad Umer Sohail
Publikováno v:
Applied Sciences, Vol 11, Iss 3706, p 3706 (2021)
Applied Sciences
Volume 11
Issue 8
Applied Sciences
Volume 11
Issue 8
Non-uniform inlet flows frequently occur in aircrafts and result in chronological distortions of total temperature and total pressure at the engine inlet. Distorted inlet flow operation of the axial compressor deteriorates aerodynamic performance, wh
Publikováno v:
2019 Sixth International Conference on Aerospace Science and Engineering (ICASE).
Honeycomb sandwich structure combines high flexural rigidity and bending strength with low weight. Sandwich structures with honeycomb as core have number of applications for aerospace, automobile and civil engineering structures. Finite element analy
Publikováno v:
Aerospace Science and Technology. 30:210-225
In this paper, we present a novel technique based upon artificial neural network (ANN), for applying aerodynamic pressure loads on the unmanned aerial vehicle (UAV) for the purpose of carrying out finite element (FE) analysis during its structural de
Autor:
Abdul Munem Khan, Imran Ali Chaudhry
Publikováno v:
Sadhana. 37:695-707
This paper explains minimization of makespan or total completion time for n-jobs, m-machine, no-wait flowshop problem (NW-FSSP). A spread sheet based general purpose genetic algorithm is proposed for the NW-FSSP. The example analysis shows that the p
Publikováno v:
International Conference on Aerospace Sciences and Aviation Technology. 12:1-11
In today’s engineering design, extensive mathematical calculations / computational analysis are done, which requires powerful engineering software to facilitate and reduce the mathematical workload. This paper pertains to the development of a compu
Publikováno v:
Mechanics of Composite Materials and Structures. 7:383-401
An investigation of a conventional propeller, made from composite materials, was conducted in which propeller characteristics were studied under quasi-static aerodynamic loading. Emphasis was placed on understanding the effects of bend-twist coupling
Autor:
Farrukh Mazhar, Abdul Munem Khan
Publikováno v:
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th.
This paper presents the structural design methodology for the wing of an Unmanned Aerial Vehicle. In this study, the application of computational methods in design is successfully explored. The strength and stiffness analysis of the UAV wing was perf