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B. K. Bharadvaj

Researcher at Douglas Aircraft Company

Publications -  12
Citations -  2134

B. K. Bharadvaj is an academic researcher from Douglas Aircraft Company. The author has contributed to research in topics: Transonic & Aerodynamics. The author has an hindex of 9, co-authored 12 publications receiving 2063 citations. Previous affiliations of B. K. Bharadvaj include Georgia Institute of Technology & Boston University.

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Journal ArticleDOI

Carotid bifurcation atherosclerosis. Quantitative correlation of plaque localization with flow velocity profiles and wall shear stress.

TL;DR: It is concluded that in the human carotid bifurcation, regions of moderate to high shear stress, where flow remains unidirectional and axially aligned, are relatively spared of intimal thickening.
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Steady flow in a model of the human carotid bifurcation. Part I--flow visualization.

TL;DR: Comparison with pathologic data on localization of atherosclerotic lesions indicates that zones susceptible to disease experience low or oscillatory shear stress while regions subject to higher shear are free of deposits.
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Steady flow in a model of the human carotid bifurcation. Part II—Laser-Doppler anemometer measurements

TL;DR: The objective of this phase of the study was to obtain quantitative information on the velocity field and to estimate levels and directions of wall shear stress in the region of the bifurcation.
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Flow studies in a model carotid bifurcation.

TL;DR: The location of atherosclerotic plaque correlates best with the low shear region of separation and not with the region of high shear at the flow divider and preliminary studies with pulsatile flow demonstrated little change from the steady flow results.
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Boundary integral equation for wave equation with moving boundary and applications to compressible potential aerodynamics of airplanes and helicopters

TL;DR: In this article, a general boundary-integral-equation methodology for the solution of the wave equation around objects moving in arbitrary motion is presented, with applications to compressible potential aerodynamics of airplanes and helicopters.