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

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

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...

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Bibliographic Details
Main Authors: , Anwar-Ul-Haque, Nugraha, Fauzul, Erawan, Dadang F, Asrar, Waqar, Sulaeman, Erwin
Format: Proceeding Paper
Language:English
English
English
Published: IEEE 2017
Subjects:
T Technology (General)
Online Access:http://irep.iium.edu.my/62919/
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

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