42nd AIAA Aerospace Sciences Meeting and Exhibit 2004
DOI: 10.2514/6.2004-252
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DNS of Attachment-line/Crossflow Boundary Layer Instability in Supersonic Swept Wing Flows

Steven E. Speer
1
,
Xiaolin Zhong
2
,
Leslie Gong
3
et al.
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Cited by 2 publications
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“…Compared with previous DNS study (Speer et al. 2004; Mack et al. 2008), the basic flow can be adequately resolved under this grid resolution.…”
Section: Basic Flowmentioning
confidence: 83%

Hypersonic attachment-line instabilities with large sweep Mach numbers

Xi
1
,
Ren
2
,
Fu
3
2021
J. Fluid Mech.
7
5
11
4
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“…Compared with previous DNS study (Speer et al. 2004; Mack et al. 2008), the basic flow can be adequately resolved under this grid resolution.…”
Section: Basic Flowmentioning
confidence: 83%

Hypersonic attachment-line instabilities with large sweep Mach numbers

Xi
1
,
Ren
2
,
Fu
3
2021
J. Fluid Mech.
7
5
11
4
View full textAdd to dashboardCite
show abstract

Boundary-layer receptivity and breakdown in hypersonic flow over a swept blunt wedge with three-dimensional freestream acoustic disturbances

Cerminara
1
,
Sandham
2
2016
8th AIAA Flow Control Conference
9
2
5
0
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