AERODYNAMICS OF AN AIRFOIL IN GROUND EFFECT WITH A JET ISSUING FROM ITS UNDERSURFACE.

Ramesh K. Agarwal; Jerry E. Deese

AERODYNAMICS OF AN AIRFOIL IN GROUND EFFECT WITH A JET ISSUING FROM ITS UNDERSURFACE.

Ramesh K. Agarwal
, Jerry E. Deese

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

Abstract

Potential flow models employing the jet-flap theory are inadequate for simulating the flowfield around an airfoil in ground effect with a jet issuing from its undersurface. Euler equations serve as a better physical model because they do not require the assumption of an infinite open wake behind the jet with pressure equal to the free-stream pressure. Airfoil/jet/ground-interaction flowfields are calculated by solving Euler equations on body-conforming curvi-linear grids.

Original language	English
Journal	AIAA Paper
State	Published - 1985

Cite this

@article{9225db666a02483baec3d9b5268e3905,

title = "AERODYNAMICS OF AN AIRFOIL IN GROUND EFFECT WITH A JET ISSUING FROM ITS UNDERSURFACE.",

abstract = "Potential flow models employing the jet-flap theory are inadequate for simulating the flowfield around an airfoil in ground effect with a jet issuing from its undersurface. Euler equations serve as a better physical model because they do not require the assumption of an infinite open wake behind the jet with pressure equal to the free-stream pressure. Airfoil/jet/ground-interaction flowfields are calculated by solving Euler equations on body-conforming curvi-linear grids.",

author = "Agarwal, \{Ramesh K.\} and Deese, \{Jerry E.\}",

year = "1985",

language = "English",

journal = "AIAA Paper",

issn = "0146-3705",

}

TY - JOUR

T1 - AERODYNAMICS OF AN AIRFOIL IN GROUND EFFECT WITH A JET ISSUING FROM ITS UNDERSURFACE.

AU - Agarwal, Ramesh K.

AU - Deese, Jerry E.

PY - 1985

Y1 - 1985

N2 - Potential flow models employing the jet-flap theory are inadequate for simulating the flowfield around an airfoil in ground effect with a jet issuing from its undersurface. Euler equations serve as a better physical model because they do not require the assumption of an infinite open wake behind the jet with pressure equal to the free-stream pressure. Airfoil/jet/ground-interaction flowfields are calculated by solving Euler equations on body-conforming curvi-linear grids.

AB - Potential flow models employing the jet-flap theory are inadequate for simulating the flowfield around an airfoil in ground effect with a jet issuing from its undersurface. Euler equations serve as a better physical model because they do not require the assumption of an infinite open wake behind the jet with pressure equal to the free-stream pressure. Airfoil/jet/ground-interaction flowfields are calculated by solving Euler equations on body-conforming curvi-linear grids.

UR - https://www.scopus.com/pages/publications/0021834192

M3 - Conference article

AN - SCOPUS:0021834192

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

AERODYNAMICS OF AN AIRFOIL IN GROUND EFFECT WITH A JET ISSUING FROM ITS UNDERSURFACE.

Abstract

Other files and links

Fingerprint

Cite this