Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Zhansen Qian"'
Publikováno v:
AIAA Journal. 61:2369-2380
Aiming at the crossflow transition problem of supersonic swept wings, an experimental study on the measurement and identification of boundary-layer stationary crossflow waves was carried out at Mach number 2.0. A 65 deg straight-swept-wing model with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c86eaceea1f691d0ea1b50190ede30a1
https://doi.org/10.2514/1.j062571
https://doi.org/10.2514/1.j062571
Publikováno v:
In Procedia Engineering 2015 99:458-476
Publikováno v:
In Procedia Engineering 2015 99:313-319
Publikováno v:
In Procedia Engineering 2015 99:129-136
Publikováno v:
Aerospace Science and Technology. 79:647-657
To compromise the compression efficiency and the starting properties, the inner contraction ratio (ICR) of a general high Mach number inlet is usually designed in the range of dual solution area. When going into an unstarted status, the high Mach inl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63c66f078eab50443dfd11e0319bd463
https://doi.org/10.1016/j.ast.2018.06.014
https://doi.org/10.1016/j.ast.2018.06.014
Publikováno v:
Applied Composite Materials. 25:921-938
Based on continuum damage mechanics (CDM), a multi-scale progressive damage model (PDM) is developed to analyze the uniaxial compression failure mechanisms of 2D triaxially braided composite (2DTBC). The multi-scale PDM starts from the micro-scale an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22865c0678ee7b1b64c3777807dbc069
https://doi.org/10.1007/s10443-018-9732-y
https://doi.org/10.1007/s10443-018-9732-y
Publikováno v:
Polymer Composites. 40:1708-1717
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8abd412d26fe3ef93b03e8cc8c544127
https://doi.org/10.1002/pc.24924
https://doi.org/10.1002/pc.24924
Publikováno v:
Advances in Effective Flow Separation Control for Aircraft Drag Reduction ISBN: 9783030296872
The effects of dielectric barrier discharge (DBD) plasma-based body force on Reynolds stresses and flow structures are studied numerically on two basic test cases, which are NACA0015 airfoil flow and backward facing step flow. The function of the pla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cd52ad811d075323b5c69ee4c11cc77
https://doi.org/10.1007/978-3-030-29688-9_6
https://doi.org/10.1007/978-3-030-29688-9_6
Publikováno v:
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b0b2eba75a3d7c730a73d7c292e3c98e
https://doi.org/10.3850/978-981-11-2730-4_0151-cd
https://doi.org/10.3850/978-981-11-2730-4_0151-cd