Half model testing for canard of a hybrid buoyant aircraft
Due to the interference effects, the intrinsic aerodynamic parameters obtained from the individual component testing are always fundamentally different than those obtained for complete model testing. Consideration and limitation for such testing need to be taken into account in any design work r...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
World Academy of Science, Engineering and Technology
2015
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/46474/1/Half-Model-Testing-for-Canard-of-a-Hybrid-Buoyant-Aircraft.pdf http://irep.iium.edu.my/46474/ http://waset.org/publications/10002489/half-model-testing-for-canard-of-a-hybrid-buoyant-aircraft |
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