Implicit multi-block Euler/Navier-Stokes simulations for hovering helicopter rotor

A three dimensional implicit multiblock Navier-Stokes solver for hovering rotor vortical flow simulations has been developed. The governing equations used are cast in an attached blade rotating frame. Two formulations of the governing equations using the relative or absolute velocity as variables re...

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Bibliographic Details
Main Author: Zhong, B.
Other Authors: Qin, N.
Language:en
Published: Cranfield University 2016
Online Access:http://dspace.lib.cranfield.ac.uk/handle/1826/10754