Adjoint aerodynamic optimization of a transonic fan rotor blade with a localized two-level mesh deformation method
Authors:
- Xiao TangXTXiao Tang
- Jiaqi LuoJLJiaqi Luo
- Feng LiuFLFeng Liu
- 1 January 2018
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 72, 267-277
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51376009, 51676003)
This publication has 19 references indexed in Scilit:
- Optimum Shape Design for Multirow Turbomachinery Configurations Using a Discrete Adjoint Approach and an Efficient Radial Basis Function Deformation Scheme for Complex Multiblock GridsJournal of Turbomachinery, 2015
- Turbine Blade Row Optimization Through Endwall Contouring by an Adjoint MethodJournal of Propulsion and Power, 2015
- A discrete adjoint harmonic balance method for turbomachinery shape optimizationAerospace Science and Technology, 2014
- Multipoint Design Optimization of a Transonic Compressor Blade by Using an Adjoint MethodJournal of Turbomachinery, 2013
- Interpretation of Adjoint Solutions for Turbomachinery FlowsAIAA Journal, 2013
- Three-Dimensional Aerodynamic Design Optimization of a Turbine Blade by Using an Adjoint MethodJournal of Turbomachinery, 2010
- Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint MethodJournal of Turbomachinery, 2010
- Automated design methodology of turbulent internal flow using discrete adjoint formulationAerospace Science and Technology, 2007
- Aerodynamic design via control theoryJournal of Scientific Computing, 1988
- Wing Design by Numerical OptimizationJournal of Aircraft, 1978