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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2020
/
Article
/
Fig 6
/
Research Article
Combustion Turbulence Flow in Trapped Vortex Combustor with Guide Vane and Blunt Body
Figure 6
Total pressure loss under different guide vanes. (a)
c
/
L
= 0.05, (b)
c
/
L
= 0.1, and (c)
c
/
L
= 0.15.
(a)
(b)
(c)