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Numerical Investigation of Shock Wave Diffraction over a Sphere Placed in a Shock Tube
- Source :
- International Journal of Aerospace Engineering, Vol 2016 (2016)
- Publication Year :
- 2016
- Publisher :
- Hindawi Publishing Corporation, 2016.
-
Abstract
- For evaluating the motion of a solid body in a gaseous medium, one has to know the drag constant of the body. It is therefore not surprising that this subject was extensively investigated in the past. While accurate knowledge is available for the drag coefficient of a sphere in a steady flow condition, the case where the flow is time dependent is still under investigation. In the present work the drag coefficient of a sphere placed in a shock tube is evaluated numerically. For checking the validity of the used flow model and its numerical solution, the present numerical results are compared with available experimental findings. The good agreement between present simulations and experimental findings allows usage of the present scheme in nonstationary flows.
- Subjects :
- Physics
Shock wave
Drag coefficient
Article Subject
lcsh:Motor vehicles. Aeronautics. Astronautics
Numerical analysis
Aerospace Engineering
Mechanics
01 natural sciences
010305 fluids & plasmas
Physics::Fluid Dynamics
Flow (mathematics)
Drag
0103 physical sciences
SPHERES
Solid body
lcsh:TL1-4050
010306 general physics
Shock tube
Subjects
Details
- Language :
- English
- ISSN :
- 16875966
- Database :
- OpenAIRE
- Journal :
- International Journal of Aerospace Engineering
- Accession number :
- edsair.doi.dedup.....bc8b65dcd397088f0834c00ad74dc0dc
- Full Text :
- https://doi.org/10.1155/2016/5740435