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Development of panel methods for subsonic analysis and designTwo computer programs, developed for subsonic inviscid analysis and design are described. The first solves arbitrary mixed analysis design problems for multielement airfoils in two dimensional flow. The second calculates the pressure distribution for arbitrary lifting or nonlifting three dimensional configurations. In each program, inviscid flow is modelled by using distributed source doublet singularities on configuration surface panels. Numerical formulations and representative solutions are presented for the programs.
Document ID
19800007773
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bristow, D. R.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3234
Report Number: NASA-CR-3234
Accession Number
80N16033
Funding Number(s)
CONTRACT_GRANT: NAS1-15369
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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