A parallel, object-oriented framework for unsteady free-wake analysis of multi-rotor/wing systems-Reference-Cited by-同舟云学术

A parallel, object-oriented framework for unsteady free-wake analysis of multi-rotor/wing systems

Published:2021-01 Issue: Volume:215 Page:104788
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Joseph Cibin,Mohan Ranjith

Funder

Indian Institute of Technology Madras

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference92 articles.

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4. Vortex Lattice Method for calculation of Quasi steady state loadings on thin elastic wings in subsonic flow;Hedman;Aeronaut Res Inst of Sweden,1966

5. Calculation of the flow around wings of arbitrary planform in a wide range of angles of attack;Belotserkovskiy;NASA TT,1969

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