Publication Date:
2019-06-28
Description:
PANAIR uses high-order panel method to predict inviscid subsonic or supersonic flows about arbitrary configuration. Panel method solves linear partial differential equation numerically by approximating configuration surface with panels on which unknown "singularity strengths" are defined. PANAIR includes advanced software technology as well as advanced aerodynamic technology.
Keywords:
MECHANICS
Type:
ARC-11398
,
NASA Tech Briefs (ISSN 0145-319X); 6; 4; P. 428
Format:
text
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