Shock tunnel investigation of boundary-layer transition at M equals 5.5

Visualization of Hypersonic Boundary Layer Transition on Elliptic Cone in High Enthalpy Shock Tunnel with Temperature-Sensitive Paint

54th AIAA Aerospace Sciences Meeting ◽

10.2514/6.2016-0358 ◽

2016 ◽

Cited By ~ 2

Author(s):

Takehiro Nagayama ◽

Hiroki Nagai ◽

Hideyuki Tanno ◽

Tomoyuki Komuro

Keyword(s):

Boundary Layer ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Temperature Sensitive ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

High Enthalpy ◽

Elliptic Cone ◽

Temperature Sensitive Paint ◽

High Enthalpy Shock Tunnel

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Experimental investigation of hypersonic boundary layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2374 ◽

2011 ◽

Cited By ~ 8

Author(s):

Alexander Wagner ◽

Viola Wartemann ◽

Stuart Laurence ◽

Jan Martinez Schramm ◽

Klaus Hannemann ◽

...

Keyword(s):

Boundary Layer ◽

Experimental Investigation ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

High Enthalpy ◽

Cone Model ◽

High Enthalpy Shock Tunnel

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Boundary-layer transition measurements in hypervelocity flows in a shock tunnel

AIAA Journal ◽

10.2514/3.15229 ◽

2002 ◽

Vol 40 ◽

pp. 1542-1548 ◽

Cited By ~ 1

Author(s):

D. J. Mee

Keyword(s):

Boundary Layer ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Layer Transition ◽

Hypervelocity Flows

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Experimental Investigation on Plate Boundary Layer Transition in JF-12 Hypersonic Shock Tunnel

Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) ◽

10.3850/978-981-11-2730-4_0091-cd ◽

2019 ◽

Author(s):

MeiKuan Liu ◽

GuiLai Han ◽

ZongLin Jiang

Keyword(s):

Boundary Layer ◽

Experimental Investigation ◽

Plate Boundary ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Layer Transition ◽

Hypersonic Shock ◽

Hypersonic Shock Tunnel

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Boundary layer transition measurements in hypervelocity flows in a shock tunnel

10.2514/6.2001-208 ◽

2001 ◽

Cited By ~ 4

Author(s):

David Mee

Keyword(s):

Boundary Layer ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Layer Transition ◽

Hypervelocity Flows

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