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

A unified unsteady flow theory of delta wings with attached shock waves
A unified unsteady flow theory of delta wings with attached shock waves
University of Southampton
Liu, D.D.
65bff81d-a05d-4305-82a2-9554e1c91e9a
Liu, D.D.
65bff81d-a05d-4305-82a2-9554e1c91e9a
East, R.A.
c31d4581-0c23-43dd-9a1e-4281dd77e32e

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)
Other
000888.PDF - Version of Record
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More information

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

Catalogue record

Date deposited: 26 Aug 2008
Last modified: 06 Jun 2019 16:31

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