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Control of shock-wave/boundary-layer interaction using abackward-facing step
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13./通讯作者:Zhai, Jian
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW(张伟为)
Adobe PDF(4533Kb)
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View/Download:283/72
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Submit date:2022/12/20
Shock-wave/boundary-layer interaction
Backward-facing step
Flow separation
Hypersonic inlet
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines
期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5./通讯作者:Zhang, Chen-An
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW
Adobe PDF(510Kb)
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Submit date:2020/08/26
Hypersonic inlet
lateral spillage
waverider design method
streamline tracing technology
mass-flow ratio
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
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Submit date:2016/09/14
Hypersonic Inlet
Shape Transition
Inward Turning
Scramjet
Design Method
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
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View/Download:1170/275
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL(李广利)
;
Qu ZP(屈志朋)
;
Situ M
;
Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/09/27
Hypersonic
Flanking Air Inlet
Waverider
Computational Fluid Dynamics(Cfd)