@inproceedings{8ddc05fef5494a70a29c7ccca3803712,
title = "Unstructured full potential analysis of a low-wing transport with nacelles",
abstract = "The need for timely and accurate analysis of engine-airframe integration issues is addressed. It is shown that the present formulation allows the analysis of wing-body-nacelle configurations to be performed in a matter of hours on typical workstation class computers. In this work a previously developed three-dimensional unstructured Full Potential formulation is used to analyze the inviscid flow field about a generic low-wing transport configuration with nacelles. The results compare favorably with the available experimental data obtained in the NASA Langley 16-Foot wind tunnel. Specifically, the nacelle-pylon-wing region flow field is accurately predicted by the present method.",
author = "Kinney, {D. J.} and Hafez, {M. M.} and Gelhausen, {P. A.}",
note = "Publisher Copyright: {\textcopyright} 1996 by the American Institute of Aeronautics and Astronautics, Inc. Ail rights reserved.; 14th Applied Aerodynamics Conference, 1996 ; Conference date: 17-06-1996 Through 20-06-1996",
year = "1996",
doi = "10.2514/6.1996-2376",
language = "English",
isbn = "9781563472121",
series = "14th Applied Aerodynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "50--60",
booktitle = "14th Applied Aerodynamics Conference",
}