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International Scholarly Research Notices
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International Scholarly Research Notices
/
2011
/
Article
/
Fig 20
/
Research Article
Preliminary Aerodynamic and Aerothermodynamic Assessment of the VTO Hopper Booster
Figure 20
Mach no. contours (a). Normalized pressure contours on vehicle surface (b). Euler computation at
𝑀
∞
=
5
,
𝛼
=
1
0
deg (a) and
𝛼
=
2
0
deg (b).
(a)
(b)