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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 1.1)

Authors :
Magnus, A. E
Epton, M. A
Publication Year :
1981
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1981.

Abstract

Panel aerodynamics (PAN AIR) is a system of computer programs designed to analyze subsonic and supersonic inviscid flows about arbitrary configurations. A panel method is a program which solves a linear partial differential equation by approximating the configuration surface by a set of panels. An overview of the theory of potential flow in general and PAN AIR in particular is given along with detailed mathematical formulations. Fluid dynamics, the Navier-Stokes equation, and the theory of panel methods were also discussed.

Subjects

Subjects :
Aerodynamics

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NAS2-9830
Publication Type :
Report
Accession number :
edsnas.19840019629
Document Type :
Report