Euler calculations of flow over a complete fighter aircraft

Ramesh K. Agarwal; Jerry E. Deese; Jerry G. Johnson; John S. Steinhoff

doi:10.2514/6.1989-2221

Euler calculations of flow over a complete fighter aircraft

Ramesh K. Agarwal
, Jerry E. Deese
, Jerry G. Johnson
, John S. Steinhoff

Research output: Contribution to conference › Paper › peer-review

Abstract

The paper describes the development of a three dimensional, Euler/Reynolds-averaged Navier-Stokes code and its application to the calculation of transonic flow about a complete fighter aircraft (wing, body, and horizontal and vertical tails assembly with fared-in inlets). Steinhoff’s blending method of grid-generation is used to generate a global grid about a generic fighter aircraft configuration. Computational results are presented for inviscid transonic flow about a fighter aircraft configuration and comparisons are made with experimental data.

Original language	English
DOIs	https://doi.org/10.2514/6.1989-2221
State	Published - 1989
Event	7th Applied Aerodynamics Conference, 1989 - Seattle, United States Duration: Jul 31 1989 → Aug 2 1989

Conference

Conference	7th Applied Aerodynamics Conference, 1989
Country/Territory	United States
City	Seattle
Period	07/31/89 → 08/2/89

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10.2514/6.1989-2221

Cite this

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title = "Euler calculations of flow over a complete fighter aircraft",

abstract = "The paper describes the development of a three dimensional, Euler/Reynolds-averaged Navier-Stokes code and its application to the calculation of transonic flow about a complete fighter aircraft (wing, body, and horizontal and vertical tails assembly with fared-in inlets). Steinhoff{\textquoteright}s blending method of grid-generation is used to generate a global grid about a generic fighter aircraft configuration. Computational results are presented for inviscid transonic flow about a fighter aircraft configuration and comparisons are made with experimental data.",

author = "Agarwal, \{Ramesh K.\} and Deese, \{Jerry E.\} and Johnson, \{Jerry G.\} and Steinhoff, \{John S.\}",

note = "Publisher Copyright: {\textcopyright} American Institute of Aeronautics and Astronautics, Inc., 1989. All rights reserved.; 7th Applied Aerodynamics Conference, 1989 ; Conference date: 31-07-1989 Through 02-08-1989",

year = "1989",

doi = "10.2514/6.1989-2221",

language = "English",

}

TY - CONF

T1 - Euler calculations of flow over a complete fighter aircraft

AU - Agarwal, Ramesh K.

AU - Deese, Jerry E.

AU - Johnson, Jerry G.

AU - Steinhoff, John S.

PY - 1989

Y1 - 1989

N2 - The paper describes the development of a three dimensional, Euler/Reynolds-averaged Navier-Stokes code and its application to the calculation of transonic flow about a complete fighter aircraft (wing, body, and horizontal and vertical tails assembly with fared-in inlets). Steinhoff’s blending method of grid-generation is used to generate a global grid about a generic fighter aircraft configuration. Computational results are presented for inviscid transonic flow about a fighter aircraft configuration and comparisons are made with experimental data.

AB - The paper describes the development of a three dimensional, Euler/Reynolds-averaged Navier-Stokes code and its application to the calculation of transonic flow about a complete fighter aircraft (wing, body, and horizontal and vertical tails assembly with fared-in inlets). Steinhoff’s blending method of grid-generation is used to generate a global grid about a generic fighter aircraft configuration. Computational results are presented for inviscid transonic flow about a fighter aircraft configuration and comparisons are made with experimental data.

UR - https://www.scopus.com/pages/publications/85006513273

U2 - 10.2514/6.1989-2221

DO - 10.2514/6.1989-2221

M3 - Paper

AN - SCOPUS:85006513273

T2 - 7th Applied Aerodynamics Conference, 1989

Y2 - 31 July 1989 through 2 August 1989

ER -

Euler calculations of flow over a complete fighter aircraft

Abstract

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