Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles

Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles

Convergent-Divergent (C-D) nozzles are used in rocket engines to produce thrust as a reaction to the acceleration of hot combustion chamber gases in the opposite direction. To maximize the engine performance at high altitudes, large area ratio, bell-shaped or contoured nozzles are used. At lower alt...

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Bibliographic Details
Main Author: Allamaprabhu, Yaravintelimath
Other Authors: Lakshmisha, K N
Language:en_US
Published: 2018
Subjects:
Rocket Nozzles
Nozzle Flow Seperation
Turbulence Modeling
Contoured Rocket Nozzles
Rocket Nozzle Flow Seperation - Numerical Simulation
Reynolds Averaged Navier-stokes (RANS) Simulations
Spalart-Allmaras (SA) Turbulence Model
Shear Stress Transport (SST) Turbulence Model
Rocket Nozzle Contours
Shear Stress Transport
SST Model
Aerospace Engineering
Online Access:http://hdl.handle.net/2005/3046
http://etd.ncsi.iisc.ernet.in/abstracts/3910/G26885-Abs.pdf

Internet

http://hdl.handle.net/2005/3046
http://etd.ncsi.iisc.ernet.in/abstracts/3910/G26885-Abs.pdf

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