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...
| Main Authors: | , , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English English English |
| Published: |
IEEE
2017
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/62919/ http://irep.iium.edu.my/62919/ 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 |
Internet
http://irep.iium.edu.my/62919/http://irep.iium.edu.my/62919/
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