Simulation Study of the Aerodynamic Force Distributions on the UAS-S45 Baalam Wing with an Upswept Blended Winglet

In this paper, the wing on the Unmanned Aerial System UAS-S45 Bàalam from Hydra Technologies is modeled and studied so that its aerodynamics and baseline performance can be better understood. More specifically, the performance of the wing, with and without a detachable upswept blended winglet, is in...

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Bibliographic Details
Main Authors: Hema AUBEELACK, Ruxandra Mihaela BOTEZ
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2019-03-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/aubeelack_botez_vol_11_iss_1.pdf
Description
Summary:In this paper, the wing on the Unmanned Aerial System UAS-S45 Bàalam from Hydra Technologies is modeled and studied so that its aerodynamics and baseline performance can be better understood. More specifically, the performance of the wing, with and without a detachable upswept blended winglet, is investigated. Using detailed CFD results, the impact of this winglet is demonstrated through its effect on the spanwise distributions of forces and moments along the wing.
ISSN:2066-8201
2247-4528