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.
Record type:
Thesis
(Doctoral)
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Published date: 1975
Organisations:
University of Southampton, Aerodynamics & Flight Mechanics
Identifiers
Local EPrints ID: 52376
URI: http://eprints.soton.ac.uk/id/eprint/52376
PURE UUID: f7a8971c-5458-4d9b-91f3-837587784789
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Date deposited: 26 Aug 2008
Last modified: 15 Mar 2024 10:36
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Contributors
Author:
D.D. Liu
Thesis advisor:
R.A. East
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