His primary scientific interests are in Mechanics, Acoustics, Boundary layer, Turbulence and Optics. Meelan M. Choudhari works mostly in the field of Mechanics, limiting it down to topics relating to Classical mechanics and, in certain cases, Vortex. Meelan M. Choudhari has researched Acoustics in several fields, including Trailing edge, Angle of attack and Edge.
His Trailing edge study incorporates themes from Aerodynamics and Vortex shedding. His Boundary layer research includes themes of Mach number and Laminar flow. His Turbulence research includes elements of Airframe, Landing gear, Wind tunnel and Noise.
Meelan M. Choudhari mainly investigates Mechanics, Boundary layer, Mach number, Reynolds number and Hypersonic speed. His research in Mechanics focuses on subjects like Classical mechanics, which are connected to Boundary value problem. His work carried out in the field of Boundary layer brings together such families of science as Surface roughness and Optics.
His Mach number study combines topics in areas such as Acoustics, Aerodynamics, Angle of attack, Freestream and Direct numerical simulation. His studies examine the connections between Reynolds number and genetics, as well as such issues in Airfoil, with regards to Leading edge. In his study, Amplitude is inextricably linked to Flow, which falls within the broad field of Turbulence.
His primary areas of study are Mechanics, Hypersonic speed, Boundary layer, Instability and Reynolds number. Meelan M. Choudhari merges Mechanics with Blunt in his study. His research integrates issues of Traveling wave, Turbulence, Numerical analysis and Wind tunnel in his study of Hypersonic speed.
His Boundary layer study combines topics from a wide range of disciplines, such as Surface finish, Laminar flow, Geometry, Nonlinear system and Surface roughness. His study in Instability is interdisciplinary in nature, drawing from both Surface, Streak, Optics and Suction. The study incorporates disciplines such as Flow separation, Computational fluid dynamics and Mach number in addition to Reynolds number.
His main research concerns Mechanics, Hypersonic speed, Mach number, Reynolds number and Laminar-turbulent transition. His study in the field of Boundary layer and Transient growth is also linked to topics like Cone and Blunt. His Boundary layer research integrates issues from Amplitude, Computation, Wavenumber and Nonlinear system.
His study explores the link between Mach number and topics such as Instability that cross with problems in Suction, Rotational symmetry, Surface, Laminar flow and Streak. His biological study deals with issues like Wind tunnel, which deal with fields such as Surface roughness. His work in Laminar-turbulent transition addresses subjects such as Angle of attack, which are connected to disciplines such as Kinetic energy, Incompressible flow and Traveling wave.
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Secondary instability of crossflow vortices and swept-wing boundary-layer transition
Mujeeb R. Malik;Fei Li;Meelan M. Choudhari;Chau-Lyan Chang.
Journal of Fluid Mechanics (1999)
Active Control of Flow-Induced Cavity Resonance
L. N. Cattafesta;S. Garg;M. Choudhari;F. Li.
28th Fluid Dynamics Conference (1997)
Computational aeroacoustic analysis of slat trailing-edge flow
Bart A. Singer;David P. Lockard;Kenneth S. Brentner;Mehdi R. Khorrami.
aiaa ceas aeroacoustics conference (1999)
Unsteady Flow Computations of a Slat with a Blunt Trailing Edge
Mehdi R. Khorrami;Mert E. Berkman;Meelan Choudhari.
AIAA Journal (2000)
A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions
Meelan Choudhari;Craig L. Streett.
Physics of Fluids (1992)
Characterization of Unsteady Flow Structures Around Tandem Cylinders for Component Interaction Studies in Airframe Noise
Luther N. Jenkins;Mehdi R. Khorrami;Meelan M. Choudhari;Catherine B. McGinley.
aiaa/ceas aeroacoustics conference (2005)
Measurements of Unsteady Wake Interference Between Tandem Cylinders
Luther N. Jenkins;Dan H. Neuhart;Cahterine B. McGinley;Meelan M. Choudhari.
36th AIAA Fluid Dynamics Conference and Exhibit (2006)
Unsteady flow computations of a slat with a blunt trailing edge
Mehdi R. Khorrami;Mert E. Berkman;Meelan Choudhari;Bart A. Singer.
aiaa ceas aeroacoustics conference (1999)
Aeroacoustic Experiments in the Langley Low-Turbulence Pressure Tunnel
Meelan M. Choudhari;David P. Lockard;Michele G. Macaraeg;Bart A. Singer.
Characterization of Unsteady Flow Structures Near Leading-Edge Slat. Part 1; PIV Measurements
Luther N. Jenkins;Mehdi R. Khorrami;Meelan Choudhari.
aiaa/ceas aeroacoustics conference (2004)
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