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…
CONTINUE READINGPosts in Category: latest news
HERE ARE OUR LATEST NEWS POSTS
Meshing and Optimization of a Vertical Axis Wind Turbine using Pointwise and CAESES
FRIENDSHIP 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 READING
Propulsion System Intake Duct for High Mach Number Regimes
Since the Wright Brothers first took to the skies over 100 years ago, the world has been completely transformed and made to feel…
CONTINUE READING