AN INVERSE METHOD FOR SUBCRITICAL FLOWS Academic Article

abstract

• The inverse problem in the tangent gas approximation is considered. An exact method for designing airfoils is presented. Constraints on the speed distribution are easily implemented. A simple numerical algorithm which is fast and accurate is presented. Comparison of designed airfoils using the tangent gas method with exact Euler results is found to be excellent for subcritical flows. 1986.

authors

• Daripa, Prabir

published proceedings

• JOURNAL OF COMPUTATIONAL PHYSICS

author list (cited authors)

• DARIPA, P. K., & SIROVICH, L.

citation count

• 7

complete list of authors

• DARIPA, PK||SIROVICH, L

publication date

• April 1986

publisher

• Elsevier  Publisher

published in

• Journal of Computational Physics  Journal

Digital Object Identifier (DOI)

• 10.1016/0021-9991(86)90196-8

start page

• 311

end page

• 328

volume

• 63

issue

• 2

URL

• http://dx.doi.org/10.1016/0021-9991(86)90196-8