A unified unsteady flow theory of delta wings with attached shock waves

Liu, D.D. (1975) A unified unsteady flow theory of delta wings with attached shock waves. University of Southampton, Department of Aeronautics and Astronautics, Doctoral Thesis , 246pp.

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Item Type:	Thesis (Doctoral)
Subjects:	T Technology > TA Engineering (General). Civil engineering (General)
Divisions:	University Structure - Pre August 2011 > School of Engineering Sciences > Aerodynamics & Flight Mechanics
Item ID:	52376
Date Deposited:	26 Aug 2008
Last Modified:	08 Jun 2012 12:23
Contributors:	Liu, D.D. (Author) East, R.A. (Thesis advisor)
Date:	1975
Status:	Unpublished
URI:	http://eprints.soton.ac.uk/id/eprint/52376

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