Apollo Capsule AS-202 Re-entry Simulation using CFD++
Flow conditions
Computations were performed for a real gas re-entry (M = 20.5, altitude = 67.3 km) of Apollo capsule AS- 202 [1] (hereafter…
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Computations were performed for a real gas re-entry (M = 20.5, altitude = 67.3 km) of Apollo capsule AS- 202 [1] (hereafter…
CONTINUE READINGFRIENDSHIP SYSTEMS investigated the aerodynamic behaviour of a vertical-axis wind turbine (VAWT) in collaboration with the US-based company Pointwise. A summary of this…
CONTINUE READINGSince the Wright Brothers first took to the skies over 100 years ago, the world has been completely transformed and made to feel…
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