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R C DiviaHarshaVardini

Observed names: DiviaHarshaVardini R C, DiviaHarshaVardini R. C., R. C. DiviaHarshaVardini, R. C.DiviaHarsha Vardini, R.C. DiviaHarshaVardini
Institution: Keimyung University
ORCID: 0000-0003-3087-6188
Observed ORCID: 0000-0003-3087-6188
OpenAlex ID: A5014002123
A hybrid genetic algorithm framework for efficient multiobjective optimization in hypersonic film cooling systems
2025 · Davood Hoseinzade, DiviaHarshaVardini R. C., et al. · Physics of Fluids · 6
An all-speed formulation using a modified γ -model for the prediction of boundary layer transition and heat transfer
2022 · DiviaHarshaVardini R C, Arul Prakash K, et al. · International Journal of Heat and Mass Transfer · 6
Genetic algorithm-based optimization of film cooling effectiveness in laminar hypersonic flow over an inclined surface
2025 · Davood Hoseinzade, DiviaHarshaVardini R C, et al. · Physics of Fluids · 5
Black-box optimization methods for hypersonic flow problems
2025 · Davood Hoseinzade, DiviaHarshaVardini R C, et al. · International Journal of Fluid Engineering · 2
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Progress in RANS-based local correlation transition models for hypersonic flows: A review
2025 · DiviaHarshaVardini R C, Ikhyun Kim · International Journal of Fluid Engineering · 2
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A numerical study of laminar/transitional shock–boundary layer interaction on a hypersonic double wedge using a modified $$\gamma $$-transition model
2024 · R. C. DiviaHarshaVardini, G. Rajesh, et al. · Shock Waves · 1
Numerical Study on Parametric Effects of Active Suction for Transition Delay in Hypersonic Boundary Layers
2025 · R.C. DiviaHarshaVardini, G. Rajesh, et al. · AIAA Journal
Assessment of Modified 𝛾-model for Hypersonic Boundary Layer Transition Prediction Considering Leading Edge Bluntness
2023 · DiviaHarshaVardini R C, Arul Prakash K, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Improved Transition Model for Hypersonic Flows by Introducing Curvature Effects
2019 · R. C.DiviaHarsha Vardini, Vinoth P, et al. · International Symposium on Shock Waves (ISSW)
Works count: 9
Citation count: 22
H-index: 3
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