An Implicit-Explicit Dirichlet-based Field Panel Method for Transonic Aircraft Design

Author:

Gebhardt Lutz1,Fokin Dmitri1,Lutz Thorsten1,Wagner Siegfried1

Affiliation:

1. University of Suttgart

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. 2Hess, J. L. "Extension of the Douglas-Neumann Program for Axisymmetric Bodies to Include Calculation of Potential, Nonuniform Cross Flow, Added Mass, and Conductor Problems," Report AD-776 639, Douglas Aircraft Company, 1964.

2. 3Maskew, B. "Program VSAERO Theory Document," NASA Contractor Report 4023, NASA, 1987.

3. PAN AIR - A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurations

4. HISSS - A higher-order subsonic/supersonic singularity method for calculating linearized potential flow

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1. Impact of Modelling Approaches on the Prediction of Ground Effect Aerodynamics;Engineering Applications of Computational Fluid Mechanics;2009-01

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