NUMERICAL SOLUTIONS OF THE EULER EQUATIONS FOR COMPLEX THREE-DIMENSIONAL AERODYNAMIC CONFIGURATIONS.

J. E. Deese; R. K. Agarwal; R. R. Underwood

doi:10.2514/6.1984-2399

NUMERICAL SOLUTIONS OF THE EULER EQUATIONS FOR COMPLEX THREE-DIMENSIONAL AERODYNAMIC CONFIGURATIONS.

J. E. Deese
, R. K. Agarwal
, R. R. Underwood

Research output: Contribution to journal › Conference article › peer-review

Abstract

An Euler code has been developed for the treatment of flowfields about several three-dimensional aircraft components. The Euler equations are solved on body-conforming curvilinear grids using an explicit Runge-Kutta time-marching finite-volume method. Grids are generated using both algebraic and elliptic partial differential equation methods. Results are presented for nacelle inlet, wing, wing-body, and wing-with-nacelle configurations. These results are compared with experimental data, solutions of the potential equation, and other Euler solutions when available.

Original language	English
Journal	AIAA Paper
DOIs	https://doi.org/10.2514/6.1984-2399
State	Published - 1984

Access to Document

10.2514/6.1984-2399

Cite this

@article{d5dfbc51658b408e87573de238c50580,

title = "NUMERICAL SOLUTIONS OF THE EULER EQUATIONS FOR COMPLEX THREE-DIMENSIONAL AERODYNAMIC CONFIGURATIONS.",

abstract = "An Euler code has been developed for the treatment of flowfields about several three-dimensional aircraft components. The Euler equations are solved on body-conforming curvilinear grids using an explicit Runge-Kutta time-marching finite-volume method. Grids are generated using both algebraic and elliptic partial differential equation methods. Results are presented for nacelle inlet, wing, wing-body, and wing-with-nacelle configurations. These results are compared with experimental data, solutions of the potential equation, and other Euler solutions when available.",

author = "Deese, \{J. E.\} and Agarwal, \{R. K.\} and Underwood, \{R. R.\}",

year = "1984",

doi = "10.2514/6.1984-2399",

language = "English",

journal = "AIAA Paper",

issn = "0146-3705",

}

TY - JOUR

T1 - NUMERICAL SOLUTIONS OF THE EULER EQUATIONS FOR COMPLEX THREE-DIMENSIONAL AERODYNAMIC CONFIGURATIONS.

AU - Deese, J. E.

AU - Agarwal, R. K.

AU - Underwood, R. R.

PY - 1984

Y1 - 1984

N2 - An Euler code has been developed for the treatment of flowfields about several three-dimensional aircraft components. The Euler equations are solved on body-conforming curvilinear grids using an explicit Runge-Kutta time-marching finite-volume method. Grids are generated using both algebraic and elliptic partial differential equation methods. Results are presented for nacelle inlet, wing, wing-body, and wing-with-nacelle configurations. These results are compared with experimental data, solutions of the potential equation, and other Euler solutions when available.

AB - An Euler code has been developed for the treatment of flowfields about several three-dimensional aircraft components. The Euler equations are solved on body-conforming curvilinear grids using an explicit Runge-Kutta time-marching finite-volume method. Grids are generated using both algebraic and elliptic partial differential equation methods. Results are presented for nacelle inlet, wing, wing-body, and wing-with-nacelle configurations. These results are compared with experimental data, solutions of the potential equation, and other Euler solutions when available.

UR - https://www.scopus.com/pages/publications/85087242757

U2 - 10.2514/6.1984-2399

DO - 10.2514/6.1984-2399

M3 - Conference article

AN - SCOPUS:85087242757

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

NUMERICAL SOLUTIONS OF THE EULER EQUATIONS FOR COMPLEX THREE-DIMENSIONAL AERODYNAMIC CONFIGURATIONS.

Abstract

Access to Document

Other files and links

Fingerprint

Cite this