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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)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.
Document ID
19840019629
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Magnus, A. E.
(Boeing Military Airplane Development Seattle, WA, United States)
Epton, M. A.
(Boeing Military Airplane Development Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
November 30, 1981
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3251
NAS 1.26:3251
Report Number: NASA-CR-3251
Report Number: NAS 1.26:3251
Accession Number
84N27697
Funding Number(s)
CONTRACT_GRANT: NAS2-9830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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