ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2019, Vol. 40 ›› Issue (8): 122740-122740.doi: 10.7527/S1000-6893.2019.22740
• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles
LI Qiang, JIANG Tao, CHEN Suyu, CHANG Yu, ZHAO Lei, ZHANG Kouli
Received:
2018-10-19
Revised:
2018-11-11
Online:
2019-08-15
Published:
2019-02-15
Supported by:
CLC Number:
LI Qiang, JIANG Tao, CHEN Suyu, CHANG Yu, ZHAO Lei, ZHANG Kouli. Measurement technique and application of boundary layer transition in shock tunnel[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(8): 122740-122740.
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Total visits: 6658907 Today visits: 1341