P
Puneet Singh
Researcher at University of Michigan
Publications - 18
Citations - 266
Puneet Singh is an academic researcher from University of Michigan. The author has contributed to research in topics: Vortex & Coaxial. The author has an hindex of 5, co-authored 17 publications receiving 195 citations. Previous affiliations of Puneet Singh include Indian Institute of Technology Kanpur.
Papers
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Reusable electrospun mesoporous ZnO nanofiber mats for photocatalytic degradation of polycyclic aromatic hydrocarbon dyes in wastewater.
TL;DR: Optimized mats of ZnO nanofibers with an average fiber diameter of 60 nm are shown to be highly effective in the photocatalytic degradation of the PAH dyes--naphthalene and anthracene.
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Application of Vortex Methods to Coaxial Rotor Wake and Load Calculations in Hover
Puneet Singh,Peretz P. Friedmann +1 more
TL;DR: The coaxial rotor has distinct advantages in hover performance and forward flight compared to a conventional isolated rotor as discussed by the authors, and the viscous vortex particle approach based on the Lagrangian formulation.
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Transient solution of the brownian coagulation equation by problem-specific polynomials
TL;DR: In this paper, an inner product with a weight function that was obtained by solving the equation of change with a constant agglomeration frequency for two different initial conditions was evaluated.
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The Global Macroeconomic Burden of Breast Cancer: Implications for Oncologic Surgery.
Kavitha Ranganathan,Puneet Singh,Krishnan Raghavendran,Edwin G. Wilkins,Jennifer B. Hamill,Oluseyi Aliu,Lisa A. Newman,David W. Hutton,Adeyiza O. Momoh +8 more
TL;DR: The global macroeconomic burden of breast cancer is quantified to underscore the critical importance of improving access to oncologic surgical care internationally and to reduce mortality and mitigate the social and financial impact of this disease in LMICs.
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Experimental Performance Evaluation of Coaxial Rotors for a Micro Aerial Vehicle
Puneet Singh,Comandur Venkatesan +1 more
TL;DR: In this paper, an experimental study performed on a coaxial-contrarotor helicopter model was performed to evaluate the performance of the rotor system using different rotor blades. But, the results of the experimental study were limited to a single-rotor configuration and the percentage thrust loss in the coaxial configuration was seen to be dependent on the ratio of the upper and lower rotor revolutions per minute as well as the spacing between the rotors.