Design of a STOL (Short Take-Off and Landing) ultralight aircraft has been carried out at Dipartimento di Ingegneria Aerospaziale (DIAS) of University of Naples by ADAG research group. Design of the aircraft has been focused on an accurate design of the high-lift system that allows very good STOL performances. In the paper all activities related to the design of the flap and slat geometries will be presented. The paper deals with the general design of flap and slat on the wing and with an accurate design of a 3-component airfoil able to achieve a maximum lift coefficient of about 4.0 in landing configuration. The numerical analysis and design activities ( airfoil and 3-D design) have been supported by deep and intensive experimental activities that have been performed in the main wind-tunnel belonging to DIAS. Many experimental results will be presented and compared to numerical predictions.
High-Lift System for STOL ultralight aircraft, design and wind-tunnel tests / Coiro, Domenico; Nicolosi, Fabrizio; DE MARCO, Agostino; Scherillo, Ferdinando; F., Grasso. - ELETTRONICO. - (2007), pp. 100-110. (Intervento presentato al convegno XIX Congresso Nazionale AIDAA tenutosi a Forlì, Italia nel 17-21 September 2007).
High-Lift System for STOL ultralight aircraft, design and wind-tunnel tests.
COIRO, DOMENICO;NICOLOSI, FABRIZIO;DE MARCO, AGOSTINO;SCHERILLO, FERDINANDO;
2007
Abstract
Design of a STOL (Short Take-Off and Landing) ultralight aircraft has been carried out at Dipartimento di Ingegneria Aerospaziale (DIAS) of University of Naples by ADAG research group. Design of the aircraft has been focused on an accurate design of the high-lift system that allows very good STOL performances. In the paper all activities related to the design of the flap and slat geometries will be presented. The paper deals with the general design of flap and slat on the wing and with an accurate design of a 3-component airfoil able to achieve a maximum lift coefficient of about 4.0 in landing configuration. The numerical analysis and design activities ( airfoil and 3-D design) have been supported by deep and intensive experimental activities that have been performed in the main wind-tunnel belonging to DIAS. Many experimental results will be presented and compared to numerical predictions.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
