Numerical Simulation of Flow around Rigid Rotor in Forward Flight

The study is devoted to the numerical simulation of flow around the rigid helicopter main rotor in forward flight based on the averaged Navier—Stokes equations in a noninertial reference frame. The calculations are performed using the in-house code NOISEtte, whose distinctive feature is the use of s...

Full description

Saved in:
Bibliographic Details
Published inFluid dynamics Vol. 55; no. 4; pp. 534 - 544
Main Authors Abalakin, I. V., Bobkov, V. G., Kozubskaya, T. K., Vershkov, V. A., Kritsky, B. S., Mirgazov, R. M.
Format Journal Article
LanguageEnglish
Published Moscow Pleiades Publishing 01.07.2020
Springer
Springer Nature B.V
Subjects
Online AccessGet full text
ISSN0015-4628
1573-8507
DOI10.1134/S0015462820040011

Cover

More Information
Summary:The study is devoted to the numerical simulation of flow around the rigid helicopter main rotor in forward flight based on the averaged Navier—Stokes equations in a noninertial reference frame. The calculations are performed using the in-house code NOISEtte, whose distinctive feature is the use of schemes with edge-based reconstruction of variables on unstructured mixed-element mesh, together with the commercial ANSYS CFX software package. The numerically obtained aerodynamic characteristics of the main rotor are compared with the data of physical experiment.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:0015-4628
1573-8507
DOI:10.1134/S0015462820040011