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Jeevani Abeygoonewardene
Jeevani Abeygoonewardene
Verified email at kdu.ac.lk - Homepage
Title
Cited by
Cited by
Year
Conceptual Design of Boom Mounted Inverted V-Tail in the Searcher MK II UAV
S Khadka, JI Abeygoonewardene, NP Liyanage
12020
Assessment of Aerodynamic Behaviour of the NACA 64A212 airfoil on the context of Computational Fluid Dynamics
R Bandara, JI Abeygoonewardena
6th International Research Conference, 2013
12013
Scaling Flight Tests of Unmanned Air Vehicles
JI Abeygoonewardene
12006
Estimation of Lift Hysteresis of an Airfoil in low speed flow
W Jayathilake, JI Abeygoonewardene
2022
Design of a Traversing Arduino Pitot Tube for the Low-speed Wind Tunnel of KDU
JI Abeygoonewardene, J Karunarathna, NRJ Thudawahewa
Uva Wellassa University of Sri Lanka, 2021
2021
Design of a traversing arduino pitot tube for the low speed wind tunnel of KDU
Abeygoonewardene, J.I., Karunarathne, J.A.D.I, Thudawahewa, N.R.J.
5th International Conference of Uva Wellassa University, Sri Lanka, 154, 2021
2021
Conceptual Design of Boom Mounted Inverted V-Tail for a UAV
NP Sushil Kadka, Abeygoonewardne, J.I., Liyanage
13th International Research Conference - KDU, 04, 2020
2020
Design of a new aircraft wing inspired by the Magnificent Frigate bird
KKSP Upasena, UI Weerathunge, JI Abeygoonewardene
Abstract Book -12th International Research Conference, 2019
2019
Impact of Human Factors on Airline Overall Maintenance Effectiveness : An Analysis of Major Aircraft Operators in Sri Lanka
JIA SH Munna, MA Hossain, KP Yapa
Abstracts - Engineering 11th International Research Conference, 23, 2018
2018
Analysis of Test section Flow conditions of Low Speed Wind Tunnel
JI Abeygoonewardene, KA Wickramasinghe, DR Caseer
10th International Conference of KDU, 2017
2017
AIRPLANE PERFORMANCE MODELLING THROUGH CFD RESULTS ASSESSMENT OF A COMPLETE 3-D WING-BODY COMBINATION
RB By: SV Abayadeera, WMUT Weerasinghe, NK Wedage, HUGT Piyarathne, JI ...
INTERNATIONAL JOURNAL FOR ADVANCE RESEARCH IN ENGINEERING AND TECHNOLOGY 3 …, 2015
2015
Airplane Performance Analysis through CFD Results: Assessment of a NACA 64A212 Wing-body Combination
RMPS Abeygoonewardene, J.I., Bandara
7th International Research Conference, 150-154, 2014
2014
Assessment of Aerodynamics of the NACA 64A212 Airfoil on the Context of Computational Fluid Dynamics
JIA RMPS Bandara
International Research Symposium, KDU: Sri Lanka as a Hub in Asia: The Way …, 2013
2013
Adaptive Control of a Missile Interceptor Control System for Optimized Performance
J Abeygoonewardene
5th International Research Conference, 183-192, 2012
2012
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