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Tiltrotor – no thoroughfare or way ahead?
, 2011 The concept of tiltrotor aircraft is nothing new. Its roots came to 1930s when the first design , which resembles to modern tiltrotors was patented. The problem was that the technology in that times was not able to support such a complex program. Only in recent years the demands for a new design combining the advantages of helicopter and aircraft in ...
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Nonlinear stability analysis of whirl flutter in a rotor-nacelle system. [PDF]
Nonlinear Dyn, 2018 Mair C, Rezgui D, Titurus B.
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Contributions of Particle Image Velocimetry to Helicopter Aerodynamics: A Review. [PDF]
AIAA J, 2017 Raffel M +5 more
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Design, Dynamics and Development of Upgraded Tiltable Wing associated Quadcopter through Advanced computational simulations incorporated Bottom-Up Approach. [PDF]
Sci RepSaravana Mohan H +9 more
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Object-guided contrastive language-image pre-training for zero-shot target recognition. [PDF]
Sci RepZheng C.
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Optimal Design of Plated/Shell Structures under Flutter Constraints-A Literature Review. [PDF]
Materials (Basel), 2019 Muc A, Flis J, Augustyn M.
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Aeroelasticity study of tiltrotor concept-whirlflutter
, 2003 In cruise flight, the tiltrotor (VSTOL) is subject to a dynamic aeroelastic instability called whirl flutter. This phenomenon is characterized by whirl movements of the rotor that increase structure load and whose consequences can be fatal. The aim of this study is to set up an analytical model allowing to accurately simulate whirl flutter.
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Aeroelastic tailoring for aerospace applications. [PDF]
HeliyonNajmi J +4 more
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