Unsteady hypersonic flow over delta wings with detached shock waves

Journal article

Peer reviewed

W. H. Hui and H. T. Hemdan

AIAA journal, Vol.14(4), pp.505-511

01/04/1976

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Title: Unsteady hypersonic flow over delta wings with detached shock waves
Creators - without role: W. H. Hui - University of Waterloo
H. T. Hemdan - University of Waterloo
Publication Details: AIAA journal, Vol.14(4), pp.505-511
Identifiers: 9951781408331
Academic Unit: King Saud University
Language: English
Resource Type: Journal article