A
Abdus Samad
Researcher at Indian Institute of Technology Madras
Publications - 149
Citations - 1932
Abdus Samad is an academic researcher from Indian Institute of Technology Madras. The author has contributed to research in topics: Turbine & Oscillating Water Column. The author has an hindex of 18, co-authored 149 publications receiving 1477 citations. Previous affiliations of Abdus Samad include Inha University & Seoul National University.
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Multiple surrogate modeling for axial compressor blade shape optimization
TL;DR: In this paper, the authors employed multiple surrogates based on the same training data to offer approximations from alternative modeling viewpoints, such as polynomial response surface approximation, Kriging, and radial basis neural network.
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Nanoemulsion gel-based topical delivery of an antifungal drug: in vitro activity and in vivo evaluation
Afzal Hussain,Abdus Samad,Sandeep Singh,Mohd Neyaz Ahsan,M W Haque,Abdul Faruk,Farhan Jalees Ahmed +6 more
TL;DR: Topical delivery of amphotericin B is suitable delivery system in NE gel carrier for skin fungal infection suggesting better alternative to painful and nephrotoxic intravenous administration.
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Design optimization of low-speed axial flow fan blade with three-dimensional RANS analysis
TL;DR: In this article, a numerical optimization procedure for a low-speed axial flow fan blade with polynomial response surface approximation model is presented, where the blade profile as well as stacking line are modified to enhance blade total efficiency.
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Multiple surrogate based optimization of a bidirectional impulse turbine for wave energy conversion
Rameez Badhurshah,Abdus Samad +1 more
TL;DR: In this article, a bidirectional impulse turbine was simulated using CFD technique and optimized using multiple surrogates approach to enhance the robustness of the optimization process by using different surrogates such as response surface approximation, radial basis function, Kriging and weighted average surrogate.
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Shape optimization of an axial compressor blade by multi-objective genetic algorithm
Abdus Samad,K-Y Kim +1 more
TL;DR: By this optimization of an axial compressor rotor blade, maximum efficiency and total pressure are increased by 1.76 and 0.41 per cent, respectively, when two extreme clustered points are considered as optimal designs.