Rinku Mukherjee
Associate Professor
+91-44 2257 4069 (Work)
Publications - 33Publications - 33
Publications - 33Publications (33)
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JournalEffect of Aerospike on Unsteady Transonic Flow over a Blunt Body
2021 | American Institute of Aeronautics and Astronautics
JournalInvestigation of Flow Separation Lines Over a Finite Wing2021 | Springer Science and Business Media Deutschland GmbH- Conferences
Study of Separation of Three-Dimensional Boundary Layer using Critical Point Theory
2021 | American Institute of Aeronautics and Astronautics - Conferences
Time Series Behaviour of Laminar Separation Bubbles at Low Reynolds Number
2021 | American Institute of Aeronautics and Astronautics Inc, AIAA - ConferencesStudy of separation of three-dimensional boundary layer using critical point theory2021 | American Institute of Aeronautics and Astronautics Inc, AIAA
- ConferencesTime series behaviour of laminar separation bubble at low reynolds number2021 | American Institute of Aeronautics and Astronautics Inc, AIAA
- Journal
Passive Control of Transonic Flow over a Blunt Body Using Aerospikes
2020 | American Institute of Aeronautics and Astronautics 
JournalExperimental validation of numerical decambering approach for flow past a rectangular wing2020 | SAGE Publications Ltd- ConferencesNumerical morphing of a rectangular wing to prevent flow separation2020 | American Institute of Aeronautics and Astronautics, Inc.
- JournalAerodynamic analysis of basic and extended lead-trail formation using numerical technique2020 | Elsevier Ltd
JournalHigh-Alfa Aerodynamics with Separated Flow Modeled as a Single Nascent Vortex2017 | Institute of Physics Publishing
Open Access- JournalDevelopment of Flow over Blunt-Nosed Slender Bodies at Transonic Mach Numbers2017 | Institute of Physics PublishingOpen Access
- JournalBehaviour of trailing wing(s) in echelon formation due to wing twist and aspect ratio2017 | Elsevier Masson SAS
- ConferencesReduction of Induced Drag in Con guration Flight using Wing Twist at Post-Stall Angles of Attack2016 | American Institute of Aeronautics and Astronautics
- ConferencesPrediction of Post-Stall Aerodynamic Characteristics of wing(s) with separated flow modeled as a Single Nascent Vortex2016 | American Institute of Aeronautics and Astronautics
- ConferencesReduction of induced drag in conguration flight using wing twist at post-stall angles of attack2016 | American Institute of Aeronautics and Astronautics Inc, AIAA
- JournalVortex interaction and roll-up in unsteady flow past tandem airfoils2016 | Isfahan University of Technology
