The analysis of flow on round-edged delta wings

Mat, Shabudin Bin (2011) The analysis of flow on round-edged delta wings. PhD thesis, University of Glasgow.

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 at speeds of 20.63 m/s and 41.23 m/s representing Reynolds numbers of 1 x 106 &

Item Type: Thesis (PhD)
Qualification Level: Doctoral
Keywords: delta wing, VFE-2, wind tunnel testing, Reynolds number and angle of attack effects
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics
Colleges/Schools: College of Science and Engineering > School of Engineering > Aerospace Sciences
Funder's Name: UNSPECIFIED
Supervisor's Name: Coton, Prof. Frank
Date of Award: 2011
Depositing User: MR shabudin Mat
Unique ID: glathesis:2011-2387
Copyright: Copyright of this thesis is held by the author.
Date Deposited: 23 Feb 2011
Last Modified: 10 Dec 2012 13:54

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