@inproceedings{40edade8f7fa4e1facd8026daaa42d26,
title = "Airfoil design via control theory using full potential and euler equations",
abstract = "This paper describes an inverse method for airfoil design. The method employs control theory to make successive perturbations to a given airfoil such that a desired pressure distribution is obtained. The flow is modeled via both the full potential and the Euler equations. Several test cases are presented to demonstrate the effectiveness of the method for aerodynamic design.",
author = "Lewis, {Jeffery C.} and Agarwal, {Ramesh K.}",
note = "Publisher Copyright: {\textcopyright} 1996 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 14th Applied Aerodynamics Conference, 1996 ; Conference date: 17-06-1996 Through 20-06-1996",
year = "1996",
language = "English",
isbn = "9781563472121",
series = "14th Applied Aerodynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "830--840",
booktitle = "14th Applied Aerodynamics Conference",
}