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International Scholarly Research Notices
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International Scholarly Research Notices
/
2011
/
Article
/
Fig 21
/
Research Article
Preliminary Aerodynamic and Aerothermodynamic Assessment of the VTO Hopper Booster
Figure 21
Pressure coefficient contours on vehicle surface with 3D streamtraces (left side). Mach no. contours on different cross planes. Euler computation at
𝑀
=
1
0
,
𝛼
=
2
0
deg.
(a)
(b)