Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability
Sign Up to like & getrecommendations! Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.03.049
Abstract: Abstract This work presents results of dynamic “one-minus-cosine” gust load simulations for a flying wing configuration. The in-house toolbox Loads Kernel is used for the loads analysis of the free flying aircraft. Flight mechanical characteristics… read more here.
Keywords: wing configuration; flying wing; open closed; flight ... See more keywords
Aerodynamic and stability analysis of personal vehicle in tandem-wing configuration
Sign Up to like & getrecommendations! Published in 2017 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410016662077
Abstract: The paper presents a concept of tandem-wing configuration aircraft that was a Warsaw University of Technology proposal for the personal air transport system. The project was developed at Warsaw University of Technology, within the PPLANE… read more here.
Keywords: wing configuration; tandem wing; analysis; vehicle ... See more keywords