Structural design of hybrid buoyant aircraft's model for subsonic wind tunnel testing

• Main Authors: , Anwar-Ul-Haque, Nugraha, Fauzul, Erawan, Dadang F, Asrar, Waqar, Sulaeman, Erwin
• Format: Conference or Workshop Item
• Language: English; English; English
• Published: IEEE 2017
• Subjects: T Technology (General)
• Online Access: http://irep.iium.edu.my/62919/1/62919%20Structural%20Design%20of%20Hybrid.pdf; http://irep.iium.edu.my/62919/2/62919%20Structural%20Design%20of%20Hybrid%20SCOPUS.pdf; http://irep.iium.edu.my/62919/13/62919%20Structural%20design%20of%20hybrid%20buoyant%20WOS.pdf; http://irep.iium.edu.my/62919/; http://ieeexplore.ieee.org/document/7868043/

In subsonic wind tunnel testing, a scaled down model should be rigid enough such that due to model deformations, there is no change in the flow field. In this regard, a computational study is carried out to analyze the stress distribution and deformation of a scaled down model of a hybrid buoya...