Zobrazeno 1 - 10
of 18
pro vyhledávání: '"S. Tauqeer ul Islam Rizvi"'
Autor:
Muhammad Suleman Malik, Naveed Iftikhar, Abdul Wadood, Muhammad Omer Khan, Muhammad Usman Asghar, Shahbaz Khan, Tahir Khurshaid, Ki-Chai Kim, Zabdur Rehman, S. Tauqeer ul Islam Rizvi
Publikováno v:
Energies, Vol 13, Iss 23, p 6169 (2020)
Renewable energy resources like solar energy, wind energy, hydro energy, photovoltaic etc. are gaining much importance due to the day by day depletion of conventional resources. Owing to the lower efficiencies of renewable energy resources, much atte
Externí odkaz:
https://doaj.org/article/78e452ef72b34b0394d8f4c7366fec0c
Publikováno v:
Defence Technology, Vol 11, Iss 4, Pp 350-361 (2015)
The objective of the paper is to compute the optimal burn-out conditions and control requirements that would result in maximum down-range/cross-range performance of a waverider type hypersonic boost-glide (HBG) vehicle within the medium and intermedi
Externí odkaz:
https://doaj.org/article/b582df87e625469dbebcc7438b8d2b9e
Autor:
Naveed Iftikhar, Zabdur Rehman, Muhammad Suleman Malik, Abdul Wadood, S. Tauqeer ul Islam Rizvi, Ki-Chai Kim, Muhammad Omer Khan, Tahir Khurshaid, Muhammad Usman Asghar, Shahbaz Khan
Publikováno v:
Energies; Volume 13; Issue 23; Pages: 6169
Energies, Vol 13, Iss 6169, p 6169 (2020)
Energies, Vol 13, Iss 6169, p 6169 (2020)
Renewable energy resources like solar energy, wind energy, hydro energy, photovoltaic etc. are gaining much importance due to the day by day depletion of conventional resources. Owing to the lower efficiencies of renewable energy resources, much atte
Publikováno v:
Defence Technology, Vol 11, Iss 4, Pp 350-361 (2015)
The objective of the paper is to compute the optimal burn-out conditions and control requirements that would result in maximum down-range/cross-range performance of a waverider type hypersonic boost-glide (HBG) vehicle within the medium and intermedi
Publikováno v:
Aircraft Engineering and Aerospace Technology. 87:67-78
Purpose – The purpose of the paper is to study the variation of optimal burnout angle at the end of the ascent phase and the optimal control deflection during the glide phase, that would maximize the downrange performance of a hypersonic boost-glid
Publikováno v:
Applied Mechanics and Materials. 390:161-165
The multiphase numerical optimization study has been carried out for a 2-stage boost vehicle and small size X-33 type lifting-body reentry vehicle with heat rate and dynamic pressure constraint. The problem has been modeled as a nonlinear, multiphase
Publikováno v:
Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST).
A wing-body re-entry vehicle has higher lift-to-drag ratio and enhances the down-range and the cross range of a ballistic vehicle. In the present study, trade-off analysis has been carried out between vehicle performance and flight parameters with va
Publikováno v:
AIP Conference Proceedings.
A numerical optimization study of lifting body re-entry vehicles is presented for nominal as well as shallow entry conditions for Medium and Intermediate Range applications. Due to the stringent requirement of a high degree of accuracy for convention
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