A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow. Part 2. Evaluation of aerodynamic influence coefficients

Title

A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow. Part 2. Evaluation of aerodynamic influence coefficients

 Author

Hoeijmakers, H.W.M.

Institution

National Aerospace Laboratory NLR

 Date

1980-12-22

 Abstract

A panel method for the computation of the velocity and pressure distribution on complex configurations in subsonic or supersonic flow has been described in Part I of the present report. This part of the report describes the evaluation of the aerodynamic influence coefficients. Expressions are derived for the (near-field) influence coefficients of the panelwise constant source distribution on the body-like components of the configuration and for the influence of the panelwise linearly varying source distribution and panelwise quadratically varying doublet distribution on the wing-like components of the configuration

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http://resolver.tudelft.nl/uuid:d3ff6299-c36e-484e-930b-280b59edbbb3

 Publisher

Nationaal Lucht- en Ruimtevaartlaboratorium

 Access restriction

Campus only

 Source

NLR-TR 80124 L Part 2

 Part of collection

Aerospace Engineering Reports

 Document type

report

 Rights

(c)1980 National Aerospace Laboratory NLR
Files
PDF NLR_TR_80124_L_PART_II.pdf 16.99 MB
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