A higher-order potential flow method for thick bodies, thin surfaces and wakes

Author:

Bernasconi D. J.,Richelsen P. M.

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference24 articles.

1. . Calculation of non-lifting potential flow about arbitrary three-dimensional bodies. Technical Report, Douglas-McDonnell, March 1962.

2. An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow. Technical Report NASA CR-2228, NASA, May 1973.

3. Calculation of potential flow about arbitrary three-dimensional lifting bodies. Final Technical Report MDC J5679-01, McDonnell Douglas, Long Beach, CA, October 1972.

4. A general panel method for the analysis and design of arbitrary configurations in incompressible flows. Technical Report NASA CR-3079, NASA, May 1980.

5. . PAN AIR—a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. Volume 1—theory document (version 3.0). Technical Report NASA CR-3251, NASA, March 1990.

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