RK
Rajan Kumar
Florida A&M University - Florida State University College of Engineering, FAMU-FSU College of Engineering, Florida State University, FAMU-FSU College of Engineering
Research areas: Engineering · Computational Mechanics · Computational Fluid Dynamics and Aerodynamics · Fluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows
Employment
- 2022 - Present
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FAMU-FSU College of Engineering, Florida State University Associate Professor2017 - 2022
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FAMU-FSU College of Engineering Assistant Professor2012 - 2017
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Florida State University Research Scientist2006 - 2012
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National Aerospace Laboratories Scientist1993 - 2006
Education
Education history is unavailable.
Projects & Funding
Projects & funding information is unavailable.
Publications (105)
- Characterization of a supersonic mixed-compression air intake at high back pressures Save
- Effect of shock impingement location on the fluid–structure interactions over a compliant panel Save
- Control of shock wave/boundary layer interactions in a supersonic air intake using a modified backward-facing step Save
- Active flow control of single and dual supersonic impinging jets using microjets Save
- Stability analysis of a supersonic flow over a modified backward facing step Save
- Role of secondary shear-layer vortices in the development of flow asymmetry on a cone–cylinder body at high angles of incidence Save
- Material Characterization of a Flat Plate with Shock Impingement: from Continuum to Atomistic Scale Save
- Active flow control of a high-lift supercritical airfoil with microjet actuators Save
- Aerodynamic characterization of barge and spar type floating offshore wind turbines at different sea states Save
- Characterization of bleedless shockwave-boundary layer interactions for high-speed intakes Save
- Characterization of independent aerodynamic effects of tail-fin deflections on an axisymmetric body Save
- Effects of a generic store on cavity resonance at supersonic speeds Save
- Experimental and numerical study of forebody vortex interactions on a generic axisymmetric finned configuration Save
- Oblique shockwave boundary layer interactions on a flexible panel at mach 2 Save
- Shock boundary layer interaction induced surface pressure field on an axisymmetric body Save
- Spatially resolved mean and unsteady surface pressure in swept SBLI using PSP Save
- Unsteady characteristics of resonant supersonic dual impinging jets Save
- Control of Flow Separation in a Rocket Nozzle Using Microjets Save
- Experimental investigation on the development of asymmetric vortices on a long slender body at high incidence Save
- Skin friction measurements using oil film interferometry in a 3-d supersonic flowfield Save