NASA NTRS · 19790000255
Advanced-panel pilot code
Abstract
Numerical research program helps establish "proof-of-concept" for newly developed higher-order panel method applicable to both subsonic and supersonic flows about nearly-arbitrary aircraft configurations. It is intended to solve variety of boundary-value problems in steady-subsonic or supersonic inviscid flow.
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Bills, G. R., Epton, M. A., Johnson, F. T.. 1979-12-01. Advanced-panel pilot code. https://ntrs.nasa.gov/citations/19790000255
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