Numerical Computation of Unsteady Compressible Flow past a Plunging Aerofoil
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Numerical Computation of Unsteady Compressible Flow past
a Plunging Aerofoil
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| Creator |
Siva Kumar , K
Sharanappa, Sajjan V |
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| Subject |
Aerodynamics
Fluid Mechanics and Thermodynamics |
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| Description |
Unsteady Reynolds-averaged Navier-Stokes (RANS) computations are presented for subsonic and transonic flow past
a plunging NACA 64A010 aerofoil. The Implicit RANS solver used for obtaining the time-accurate solution is based
on finite volume nodal point spatial discretization scheme with dual time stepping. Results for the subsonic and
transonic cases compare well with the experimental data, thus demonstrating the capability of the solver to provide
useful unsteady pressure data for aeroelastic analysis.
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| Publisher |
Regional Information Center for Science and Technology
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| Date |
2012
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| Type |
Journal Article
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/11718/1/19471_030513094723.pdf
Siva Kumar , K and Sharanappa, Sajjan V (2012) Numerical Computation of Unsteady Compressible Flow past a Plunging Aerofoil. Journal of Applied Fluid Mechanics, 5 (4). pp. 131-138. ISSN 1735-3572 |
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| Relation |
http://jafmonline.net/web/guest/home
http://nal-ir.nal.res.in/11718/ |
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