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$12 USD / hora
Bandera de SRI LANKA
kurunegala, sri lanka
$12 USD / hora
Aquí son las 8:42 a. m.
Se unió el julio 20, 2017
0 Recomendaciones

Uditha G.

@udithag

 5,0 (2 comentarios)
2,8
2,8
100%
100%
$12 USD / hora
Bandera de SRI LANKA
kurunegala, sri lanka
$12 USD / hora
100 %
Trabajos finalizados
100 %
Dentro del presupuesto
100 %
A tiempo
N/A
Tasa de recontratación

Aerospace Engineer & Forex Trader

I completed my BSc Engineering Degree from the University of Moratuwa from the field of Mechanical Engineering in 2013 and Since then I am working as a Research Engineer in a Medium Range UAV developent project. I do designing new Airframes, Analysing Aerodynamic properties, Stress analysis , Finite elemet analysis and lot of stuff related to Mathematics ,Physics and Mechanical Engineering designs. I was also a member of the Sri Lankan Physics Olympiad Squad in 2008. I am very much interested in doing calculations related to mathematics and physics Since 2011, I have been trading in the forex market and have done a lot of research about how forex market works. I have developed some Expert Advisers for some currency pairs with successful unconventional stratergies. I do mql4 programming as a hobby
Freelancer Aeronautical Engineers Sri Lanka
Ver todo Aeronautical Engineers en Sri Lanka

Contacta Uditha G. sobre tu trabajo

Inicia sesión para comentar cualquier detalle por chat.

Portafolio

4408187
Wing Structure
4405748
First Flight of Hand Launched UAV with V-tail configuration
Hand Launched UAV First Flight
4405729
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
4405708
Solidworks was used to Calculate Stresses and Shear forces of the wing and also the deflection Wing was modeled as a Composite part made of Carbon fiber
Finite Element Analysis of a Composite Wing
Solidworks was used to Calculate Stresses and Shear forces of the wing and also the deflection Wing was modeled as a Composite part made of Carbon fiber
Finite Element Analysis of a Composite Wing
4405537
TOW = 48kg Wing Span = 15.6 ft Length = 11ft Wing area = 1.4 m^2 Power plant = 8.2 hp Cruising speed = 53 kts Stall speed = 39 kts
Medium Range UAV
TOW = 48kg Wing Span = 15.6 ft Length = 11ft Wing area = 1.4 m^2 Power plant = 8.2 hp Cruising speed = 53 kts Stall speed = 39 kts
Medium Range UAV
4405520
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
4408187
Wing Structure
4405748
First Flight of Hand Launched UAV with V-tail configuration
Hand Launched UAV First Flight
4405729
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
GCS was modeled using Solidworks sheet metal and manufactured
Ground Control Station
4405708
Solidworks was used to Calculate Stresses and Shear forces of the wing and also the deflection Wing was modeled as a Composite part made of Carbon fiber
Finite Element Analysis of a Composite Wing
Solidworks was used to Calculate Stresses and Shear forces of the wing and also the deflection Wing was modeled as a Composite part made of Carbon fiber
Finite Element Analysis of a Composite Wing
4405537
TOW = 48kg Wing Span = 15.6 ft Length = 11ft Wing area = 1.4 m^2 Power plant = 8.2 hp Cruising speed = 53 kts Stall speed = 39 kts
Medium Range UAV
TOW = 48kg Wing Span = 15.6 ft Length = 11ft Wing area = 1.4 m^2 Power plant = 8.2 hp Cruising speed = 53 kts Stall speed = 39 kts
Medium Range UAV
4405520
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project
Takeoff Weight Estimation Aircraft Sizing Numerical Model Aerodynamic Characteristics V-n Diagram Wing Loads Wing Structure
Aircraft Design Project

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5,0
£170,00 GBP
Project 24057739 has been deleted
Very patient and understanding with non-experts. A pleasure to work with Uditha!
Avatar del usuario
Bandera de Victor C.
@vcovasan1
•
hace 4 años
5,0
£20,00 GBP
Project for Uditha G.
Very helpful. Delivered my work on time, has excellent knowledge and outstanding skills.
Metatrader
Aeronautical Engineering
Linear Programming
Physics
+1 más
A
Closed User
@Ai090
•
hace 4 años

Educación

BSc Engineering

University of Moratuwa, Sri Lanka 2008 - 2013
(5 años)

Contacta Uditha G. sobre tu trabajo

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Principales habilidades

Aeronautical Engineering 2
Metatrader 1
Aerospace Engineering 1
Linear Programming 1
Physics 1

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