Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet

Namkyu Lee; Ji Yeul Bae; Jiwoon Song; Taehwan Kim; Yoon Goo Kang; Hyunghee Cho

Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet

Namkyu Lee, Ji Yeul Bae, Jiwoon Song, Taehwan Kim, Yoon Goo Kang, Hyunghee Cho

Department of Mechanical Engineering

Research output: Contribution to conference › Paper › peer-review

Original language	English
Publication status	Published - 2014
Event	15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014 - Honolulu, United States Duration: 2014 Feb 24 → 2014 Feb 28

Other

Other	15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014
Country/Territory	United States
City	Honolulu
Period	14/2/24 → 14/2/28

All Science Journal Classification (ASJC) codes

Mechanical Engineering

Cite this

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title = "Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet",

author = "Namkyu Lee and Bae, {Ji Yeul} and Jiwoon Song and Taehwan Kim and Kang, {Yoon Goo} and Hyunghee Cho",

year = "2014",

language = "English",

note = "15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014 ; Conference date: 24-02-2014 Through 28-02-2014",

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Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet. / Lee, Namkyu; Bae, Ji Yeul; Song, Jiwoon et al.

2014. Paper presented at 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014, Honolulu, United States.

Research output: Contribution to conference › Paper › peer-review

TY - CONF

T1 - Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet

AU - Lee, Namkyu

AU - Bae, Ji Yeul

AU - Song, Jiwoon

AU - Kim, Taehwan

AU - Kang, Yoon Goo

AU - Cho, Hyunghee

PY - 2014

Y1 - 2014

UR - http://www.scopus.com/inward/record.url?scp=84914133115&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84914133115&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:84914133115

T2 - 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014

Y2 - 24 February 2014 through 28 February 2014

ER -

Thermal analysis by shock and boundary layer interaction in the supersonic flow with penetration jet

Other

All Science Journal Classification (ASJC) codes

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Cite this