The purpose of this work is to provide a comprehensive overview of JPAD (Java toolchain of Programs for Aircraft Design), a java-based framework conceived as a fast and efficient tool useful as support in the preliminary design phases of an aircraft, and during its optimization process. The software platform is made to perform fast multi-disciplinary analysis of an established aircraft configuration and to search for an optimized configuration in a domain, whose boundaries are defined by the user. The following sections will focus on the description of the software structure and on the results obtained from a case study carried out assuming as baseline a regional turboprop aircraft model similar to ATR-72.

A Java toolchain of programs for aircraft design / De Marco, A; Cusati, V; Trifari, Vittorio; Ruocco, M; Nicolosi, F; Della Vecchia, P.. - Unico:(2017), pp. 1-16. (Intervento presentato al convegno 6th CEAS Air and Space Conference tenutosi a Bucharest (ROMANIA) nel 16-20 October, 2017).

A Java toolchain of programs for aircraft design

De Marco A;Cusati V;Trifari, Vittorio;Ruocco M;Nicolosi F;Della Vecchia P.
2017

Abstract

The purpose of this work is to provide a comprehensive overview of JPAD (Java toolchain of Programs for Aircraft Design), a java-based framework conceived as a fast and efficient tool useful as support in the preliminary design phases of an aircraft, and during its optimization process. The software platform is made to perform fast multi-disciplinary analysis of an established aircraft configuration and to search for an optimized configuration in a domain, whose boundaries are defined by the user. The following sections will focus on the description of the software structure and on the results obtained from a case study carried out assuming as baseline a regional turboprop aircraft model similar to ATR-72.
2017
978-973-0-25597-3
A Java toolchain of programs for aircraft design / De Marco, A; Cusati, V; Trifari, Vittorio; Ruocco, M; Nicolosi, F; Della Vecchia, P.. - Unico:(2017), pp. 1-16. (Intervento presentato al convegno 6th CEAS Air and Space Conference tenutosi a Bucharest (ROMANIA) nel 16-20 October, 2017).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/696606
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