Method and system for a quick calculation of aerodynamic forces on an aircraft

A computer-aided method suitable for assisting in the design of an aircraft by providing the dimensioning aerodynamic forces and other relevant values comprising the following steps: a) Selecting a set of parameters of the aircraft, being said aerodynamic forces and other relevant values dependant o...

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Bibliographische Detailangaben
Hauptverfasser: ALONSO FERNANDEZ DIEGO, VELAZQUEZ LOPEZ ANGEL GERARDO, VEGA DE PRADA JOSE MANUEL, LORENTE MANZANARES LUIS SANTIAGO
Format: Patent
Sprache:eng
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