Rotor-Fuselage-Intake Aerodynamics and Icing Using Vortex and Eulerian–Lagrangian Computational Fluid Dynamics Methods
Bidesh Sengupta(University of Bologna), L. Prince Raj(Lovely Professional University), Hakjin Lee(Gyeongsang National University), Esmaeil Esmaeilifar(Gyeongsang National University), M. Sadegh Araghizadeh(Gyeongsang National University), R.S. Myong(Gyeongsang National University)
Cited by 7
Related Papers
Ice accretion and aerodynamic effects on a multi-element airfoil under SLD icing conditions
|Aerospace Science and Technology|2018|88
Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing
|Aerospace Science and Technology|2020|77
Performance evaluation of electrothermal anti-icing systems for a rotorcraft engine air intake using a meta model
|Aerospace Science and Technology|2020|36
A super-parallel mixed explicit discontinuous Galerkin method for the second-order Boltzmann-based constitutive models of rarefied and microscale gases
|Computers & Fluids|2017|32
Computational simulation of ice accretion and shedding trajectory of a rotorcraft in forward flight with strong rotor wakes
|Aerospace Science and Technology|2021|27