Mixed Jameson/total-variation-diminishing scheme applied to simulating rotor airfoil flowfield

Yihua Cao; Jifei Wang; Yuan Su

doi:10.2514/2.3080

Mixed Jameson/total-variation-diminishing scheme applied to simulating rotor airfoil flowfield

Yihua Cao^*
, Jifei Wang
, Yuan Su

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

10 Scopus citations

Abstract

A mixed Jameson/total-variation diminishing scheme applied to simulating rotor airfoil flowfield was presented. The scheme is used to solve the Euler equations for the simulation of the flowfield around a rotor airfoil. Considering the Euler equations' deficiency in reflecting viscous effects, Jameson's scheme was applied to solve the Navier-Stokes equations. Results of the calculation and experimental data were found in good agreement for Caradonna and Tung's rotor blades.

Original language	English
Pages (from-to)	213-216
Number of pages	4
Journal	Journal of Aircraft
Volume	40
Issue number	1
DOIs	https://doi.org/10.2514/2.3080
State	Published - 2003

Access to Document

10.2514/2.3080

Cite this

@article{23b0af7f3c1841849fd70f44566c16bd,

title = "Mixed Jameson/total-variation-diminishing scheme applied to simulating rotor airfoil flowfield",

abstract = "A mixed Jameson/total-variation diminishing scheme applied to simulating rotor airfoil flowfield was presented. The scheme is used to solve the Euler equations for the simulation of the flowfield around a rotor airfoil. Considering the Euler equations' deficiency in reflecting viscous effects, Jameson's scheme was applied to solve the Navier-Stokes equations. Results of the calculation and experimental data were found in good agreement for Caradonna and Tung's rotor blades.",

author = "Yihua Cao and Jifei Wang and Yuan Su",

year = "2003",

doi = "10.2514/2.3080",

language = "英语",

volume = "40",

pages = "213--216",

journal = "Journal of Aircraft",

issn = "0021-8669",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "1",

}

TY - JOUR

T1 - Mixed Jameson/total-variation-diminishing scheme applied to simulating rotor airfoil flowfield

AU - Cao, Yihua

AU - Wang, Jifei

AU - Su, Yuan

PY - 2003

Y1 - 2003

N2 - A mixed Jameson/total-variation diminishing scheme applied to simulating rotor airfoil flowfield was presented. The scheme is used to solve the Euler equations for the simulation of the flowfield around a rotor airfoil. Considering the Euler equations' deficiency in reflecting viscous effects, Jameson's scheme was applied to solve the Navier-Stokes equations. Results of the calculation and experimental data were found in good agreement for Caradonna and Tung's rotor blades.

AB - A mixed Jameson/total-variation diminishing scheme applied to simulating rotor airfoil flowfield was presented. The scheme is used to solve the Euler equations for the simulation of the flowfield around a rotor airfoil. Considering the Euler equations' deficiency in reflecting viscous effects, Jameson's scheme was applied to solve the Navier-Stokes equations. Results of the calculation and experimental data were found in good agreement for Caradonna and Tung's rotor blades.

UR - https://www.scopus.com/pages/publications/0037228170

U2 - 10.2514/2.3080

DO - 10.2514/2.3080

M3 - 文章

AN - SCOPUS:0037228170

SN - 0021-8669

VL - 40

SP - 213

EP - 216

JO - Journal of Aircraft

JF - Journal of Aircraft

IS - 1

ER -

Mixed Jameson/total-variation-diminishing scheme applied to simulating rotor airfoil flowfield

Abstract

Access to Document

Other files and links

Fingerprint

Cite this