Turbulent-flow calculations for flow over wings near maximum lift

J. E. Deese; R. K. Agarwal

Turbulent-flow calculations for flow over wings near maximum lift

J. E. Deese
, R. K. Agarwal

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

Abstract

Calculation of horizontal-stabllizer flowfields near maximum lift using a three-dimensional Navier-Stokes code is described. Results are presented for two stabilizer configurations with and without elevator deflection. Predicted lift coefficients are within 10% of experimental values up to the onset of stall. The code is able to predict the onset of both wing and elevator stall for the two configurations studied. Surface pressure distribution predictions are in good agreement with experimental data.

Original language	English
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

Cite this

@conference{c3aac8ed4abf4717866b9153c2726014,

title = "Turbulent-flow calculations for flow over wings near maximum lift",

abstract = "Calculation of horizontal-stabllizer flowfields near maximum lift using a three-dimensional Navier-Stokes code is described. Results are presented for two stabilizer configurations with and without elevator deflection. Predicted lift coefficients are within 10\% of experimental values up to the onset of stall. The code is able to predict the onset of both wing and elevator stall for the two configurations studied. Surface pressure distribution predictions are in good agreement with experimental data.",

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

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",

language = "English",

}

TY - CONF

T1 - Turbulent-flow calculations for flow over wings near maximum lift

AU - Deese, J. E.

AU - Agarwal, R. K.

PY - 1989

Y1 - 1989

N2 - Calculation of horizontal-stabllizer flowfields near maximum lift using a three-dimensional Navier-Stokes code is described. Results are presented for two stabilizer configurations with and without elevator deflection. Predicted lift coefficients are within 10% of experimental values up to the onset of stall. The code is able to predict the onset of both wing and elevator stall for the two configurations studied. Surface pressure distribution predictions are in good agreement with experimental data.

AB - Calculation of horizontal-stabllizer flowfields near maximum lift using a three-dimensional Navier-Stokes code is described. Results are presented for two stabilizer configurations with and without elevator deflection. Predicted lift coefficients are within 10% of experimental values up to the onset of stall. The code is able to predict the onset of both wing and elevator stall for the two configurations studied. Surface pressure distribution predictions are in good agreement with experimental data.

UR - https://www.scopus.com/pages/publications/85006507928

M3 - Paper

AN - SCOPUS:85006507928

T2 - 7th Applied Aerodynamics Conference, 1989

Y2 - 31 July 1989 through 2 August 1989

ER -

Turbulent-flow calculations for flow over wings near maximum lift

Abstract

Conference

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