[E-Project] Study of the most suitable wing configuration for STOL operations
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hdl:2117/175375
Document typeBachelor thesis
Date2017-06
Rights accessRestricted access - author's decision
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Abstract
he aim of this project is to study, analyse and develop a wing configuration intended to perform STOL operations. The developed wing should be suitable for its use in the electriclightweight aircraft currently being developed in the E-Project. Furthermore, along with the development of the wing, this project is intended to provide a complete study of thewing configuration parameters effect on the aerodynamic behaviour of the wing for future improvements.
Description
The target of this study is find the most adequate wing configuration for short take-off and landing operations with a light aircraft.
SubjectsShort take-off and landing aircraft--Design and construction, Airplanes--Wings--Design and construction, Electric airplanes, Avions -- Disseny i construcció, Avions -- Ales -- Disseny, Avions elèctrics
DegreeGRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS (Pla 2010)
Files | Description | Size | Format | View |
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REPORT_354.pdf![]() | 3,438Mb | Restricted access | ||
ANNEX_241.pdf![]() | 7,049Mb | Restricted access | ||
BUDGET_366.pdf![]() | 404,7Kb | Restricted access |