Higher-Order Panel Method for Aerodynamic Flow Analysis

L. L. Erickson,R. L. Carmichael,A. D. Levin,A. Magnus,M Epton,P. Baruah,B. Massena,John E. Bussoletti,K. W. Sidwell,F. Johnson,J. Zeppa,G. Bates,D. Clemens,T. Derbyshire,D. Purdon,D Chiang,P. Rubbert,F. Nelson,J Wai,K. Tsurusaki,N. Smith,J. R. Snyder,W. Sotomayer,J. Dejongh,J. L. Thomas

Higher-Order Panel Method for Aerodynamic Flow Analysis

1982

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:

Aerospace engineering
Aerodynamics
Airfoil
Physics
Mathematics
panel method
Partial differential equation
Flow (psychology)
Supersonic speed
Inviscid flow
Singularity
Mathematical analysis

Correction
Source
Cite
Save
Machine Reading By IdeaReader

References

Citations