EFFECT OF KNUDSEN NUMBER ON BLUNT BODY DURING HYPERSONIC SPEEDS FOR REDUCING DRAG
Posted on 18 Sep 2020 11:29 pm
A deep study is performed to calculate the particle behavior of the fluid on the blunt-body which is traveling in Hypersonic speed of Mach 6, 6.5, 7, 7.5, 8. A deep understanding of the thermal load is studied. This paper helps in studying the nonequilibrium condition of the fluid behavior by varying Knudnes Number.
Software
FLUENT
ICEM CFD
PTC Creo Parametric
Categories
Aerospace
Design
Keywords
Knudsen Number
Equilibrium and NonEquilibrium Loads
Thermal Loads
Hypersonic Speeds
Blunt Nosed Body
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