Inverse aerodynamic design method for aircraft components

Inverse aerodynamic design method for aircraft components

An existing, semi-inverse, aerodynamic design algorithm is modified to permit the unrestricted geometric design of aircraft components with prescribed aerodynamic surface pressures. A brief description of the present design procedure is given and computed results are presented for both a two-dimensi...

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Veröffentlicht in:Journal of aircraft 1987-01, Vol.24 (1), p.8-9
Hauptverfasser: Malone, J. B, Vadyak, J, Sankar, L. N
Format: Artikel
Sprache:eng
Schlagworte:
aerodynamics
aircraft components
airfoils
computer aided design
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Beschreibung
Zusammenfassung:An existing, semi-inverse, aerodynamic design algorithm is modified to permit the unrestricted geometric design of aircraft components with prescribed aerodynamic surface pressures. A brief description of the present design procedure is given and computed results are presented for both a two-dimensional airfoil and a three-dimensional nacelle configuration.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.45403