A low cost prototyping approach for design analysis and flight testing of the TURAC VTOL UAV

Author(s):  
Yucel Orkut Aktas ◽  
Ugur Ozdemir ◽  
Yasin Dereli ◽  
Ahmed Farabi Tarhan ◽  
Aykut Cetin ◽  
...  
Aerospace ◽  
2021 ◽  
Vol 8 (3) ◽  
pp. 74
Author(s):  
Alejandro Sobron ◽  
David Lundström ◽  
Petter Krus

Testing of untethered subscale models, often referred to as subscale flight testing, has traditionally had a relatively minor, yet relevant use in aeronautical research and development. As recent advances in electronics, rapid prototyping and unmanned-vehicle technologies expand its capabilities and lower its cost, this experimental method is seeing growing interest across academia and the industry. However, subscale models cannot meet all similarity conditions required for simulating full-scale flight. This leads to a variety of approaches to scaling and to other alternative applications. Through a literature review and analysis of different scaling strategies, this study presents an overall picture of how subscale flight testing has been used in recent years and synthesises its main issues and practical limitations. Results show that, while the estimation of full-scale characteristics is still an interesting application within certain flight conditions, subscale models are progressively taking a broader role as low-cost technology-testing platforms with relaxed similarity constraints. Different approaches to tackle the identified practical challenges, implemented both by the authors and by other organisations, are discussed and evaluated through flight experiments.


2013 ◽  
Vol 15 (AEROSPACE SCIENCES) ◽  
pp. 1-10
Author(s):  
M. Zakaria ◽  
A. Hammad ◽  
M. Moattasem
Keyword(s):  
Low Cost ◽  

10.14311/242 ◽  
2001 ◽  
Vol 41 (4-5) ◽  
Author(s):  
C. Munro ◽  
P. Krus

Conceptual aircraft design is characterised by the requirement to analyse a large number of configurations rapidly and cost effectively. For unusual configurations such as those typified by unmanned combat air vehicles (UCAVs) adequately predicting their aerodynamic characteristics through existing empirical methods is fraught with uncertainty. By utilising rapid and low cost experimental tools such as the water tunnel and subscale flight testing it is proposed that the required aerodynamic characteristics can rapidly be acquired with sufficient fidelity for the conceptual design phase. Furthermore, the initial design predictions can to some extent be validated using flight-derived aerodynamic data from subscale flight testing.


Nanoscale ◽  
2021 ◽  
Author(s):  
Roy Avrahamy ◽  
Benny Milgrom ◽  
Moshe Zohar ◽  
Mark Auslender

The demand for miniature, low-cost, utmost efficient optical absorbers triggered ongoing research efforts to minimize the overall design thickness, particularly the photo-active layer, while still maintaining a high optical absorptance....


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