Shock-wave/boundary-layer interaction at a swept compression corner

Oktay Özcan; M. Orhan Kaya

doi:10.2514/3.10314

Shock-wave/boundary-layer interaction at a swept compression corner

Oktay Özcan
, M. Orhan Kaya

Department of Aeronautical Engineering

Istanbul Technical University
National Aeronautics and Space Administration

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Original language	English
Pages (from-to)	1646-1648
Number of pages	3
Journal	AIAA Journal
Volume	27
Issue number	11
DOIs	https://doi.org/10.2514/3.10314
Publication status	Published - Nov 1989

Funding

This study was supported by the UYG-AR Applied Research Center of Istanbul Technical University.

Funders
UYG-AR
Istanbul Teknik Üniversitesi

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10.2514/3.10314

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title = "Shock-wave/boundary-layer interaction at a swept compression corner",

author = "Oktay {\"O}zcan and Kaya, \{M. Orhan\}",

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AU - Kaya, M. Orhan

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Shock-wave/boundary-layer interaction at a swept compression corner

Funding

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