Design optimization of rocket nozzles in chemically reacting flows

DOI10.1016/J.COMPFLUID.2012.05.002zbMath1365.76334OpenAlexW2023655872MaRDI QIDQ2361887

S. Eyi, Mine Yumuşak

Publication date: 5 July 2017

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2012.05.002

zbMATH Keywords

design optimizationreacting flowsadjoint methodrocket's nozzle

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Reaction effects in flows (76V05)

Related Items (2)

Design optimization of rocket nozzles in chemically reacting flows ⋮ Analysis and design optimization of solid rocket motors in viscous flows

Uses Software

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Cites Work

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• Inviscid flux-splitting algorithms for real gases with non-equilibrium chemistry
• Airfoil design optimization using the Navier-Stokes equations
• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• Design optimization of rocket nozzles in chemically reacting flows
• Performance Evaluation of the Numerical Flux Jacobians in Flow Solution and Aerodynamic Design Optimization
• Performance prediction and optimization for liquid rocket engine nozzle
• Effects of the Jacobian evaluation on Newton's solution of the Euler equations

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