A comparison of plunging- and pitching-induced deep dynamic stall on an SD7003 airfoil using URANS and LES simulations-Reference-Cited by-同舟云学术

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A comparison of plunging- and pitching-induced deep dynamic stall on an SD7003 airfoil using URANS and LES simulations

Published:2022-02 Issue: Volume:121 Page:107307
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Carta Mario^ORCID,Putzu Roberto^ORCID,Ghisu Tiziano^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference83 articles.

1. Numerical investigation of deep dynamic stall for a helicopter blade section;Wen;AIAA J.,2019

2. Control of rotorcraft retreating blade stall using air-jet vortex generators;Singh;J. Aircr.,2006

3. The phenomenon of dynamic stall;McCroskey,1981

4. An analysis of the stall flutter instability of helicopter rotor blades;Carta;J. Am. Helicopter Soc.,1967

5. Unsteady aerodynamic forces on NACA 0015 airfoil in harmonic translatory motion;Gaunaa,2002

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4. Large eddy simulation of cavitating flow around a pitching hydrofoil;Ocean Engineering;2024-01

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