Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties
-
Fan Yang
Abstract
This work presents an approach for sensitivity analysis of turbine cooling blade with surface thickness uncertainties, combining mesh deformation method, neural network model and multidisciplinary analysis. Normally, for even tiny shape changes, conventional geometry-based method failed easily during the auto-processing analysis. Therefore, mesh deformation method was utilized to capture the tiny size changes in the multidisciplinary analysis for both the fluid and the structure meshes. The neural network model is constructed by design of experiments to reduce the computational cost. Sensitivity analysis of the multidisciplinary system of blade is performed by numerical difference algorithm with the neural network model. Results showed that the proposed method was effective and practical in engineering.
Funding source: Natural Science Foundation of Jiangsu Province
Award Identifier / Grant number: BK20190424
Funding source: National Natural Science Foundation of China
Award Identifier / Grant number: 51975471
Funding source: Natural Science Foundation of Shanghai
Award Identifier / Grant number: 21ZR1469300
Funding source: Shaanxi Science Foundation for Distinguished Young Scholars
Award Identifier / Grant number: 2022JC-36
-
Author contributions: All the authors have accepted responsibility for the entire content of this submitted manuscript and approved submission.
-
Research funding: This work was supported by the Natural Science Foundation of Jiangsu Province (BK20190424), National Natural Science Foundation of China (51975471), Natural Science Foundation of Shanghai (21ZR1469300) and Shaanxi Science Foundation for Distinguished Young Scholars (2022JC-36).
-
Declaration of conflicting interests: The authors declared no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.
References
1. Sobieszczanski-Sobieski, J, Haftka, RT. Multidisciplinary aerospace design optimization: survey of recent developments. Struct Optim 1997;14:1–23. https://doi.org/10.1007/bf01197554.Search in Google Scholar
2. Yu, K, Yang, X, Yue, Z. Aerodynamic and heat transfer design optimization of internally cooling turbine blade based different surrogate models. Struct Multidiscip Optim 2011;44:75–83. https://doi.org/10.1007/s00158-010-0583-x.Search in Google Scholar
3. Ashuri, T, Zaaijer, MB, Martins, JR, Van Bussel, GJ, Van Kuik, GA. Multidisciplinary design optimization of offshore wind turbines for minimum levelized cost of energy. Renew Energy 2014;68:893–905. https://doi.org/10.1016/j.renene.2014.02.045.Search in Google Scholar
4. Meng, D, Liu, M, Yang, S, Zhang, H, Ding, R. A fluid–structure analysis approach and its application in the uncertainty-based multidisciplinary design and optimization for blades. Adv Mech Eng 2018;10:1687814018783410. https://doi.org/10.1177/1687814018783410.Search in Google Scholar
5. Afonso, F, Vale, J, Lau, F, Suleman, A. Performance based multidisciplinary design optimization of morphing aircraft. Aero Sci Technol 2017;67:1–12. https://doi.org/10.1016/j.ast.2017.03.029.Search in Google Scholar
6. Benaouali, A, Kachel, S. Multidisciplinary design optimization of aircraft wing using commercial software integration. Aero Sci Technol 2019;92:766–76. https://doi.org/10.1016/j.ast.2019.06.040.Search in Google Scholar
7. York, MA, Öztürk, B, Burnell, E, Hoburg, WW. Efficient aircraft multidisciplinary design optimization and sensitivity analysis via signomial programming. AIAA J 2018;56:4546–61. https://doi.org/10.2514/1.j057020.Search in Google Scholar
8. Sgueglia, A, et al.. Multidisciplinary design optimization framework with coupled derivative computation for hybrid aircraft. J Aircraft 2020;57:715–29. https://doi.org/10.2514/1.c035509.Search in Google Scholar
9. Oh, S, Jiang, CH, Jiang, C, Marcus, PS. Finding the optimal shape of the leading-and-trailing car of a high-speed train using design-by-morphing. Comput Mech 2018;62:23–45. https://doi.org/10.1007/s00466-017-1482-4.Search in Google Scholar
10. Silvas, E, Hofman, T, Murgovski, N, Etman, LP, Steinbuch, M. Review of optimization strategies for system-level design in hybrid electric vehicles. IEEE Trans Veh Technol 2016;66:57–70. https://doi.org/10.1109/tvt.2016.2547897.Search in Google Scholar
11. Miao, B, Luo, Y, Qiu, Y, Peng, Q, Jiang, C, Yang, Z. Research on multidisciplinary fatigue optimization design method in structural design of high speed train. Procedia Struct Integr 2019;22:102–9. https://doi.org/10.1016/j.prostr.2020.01.014.Search in Google Scholar
12. Alba, C, Elham, A, German, BJ, Veldhuis, LL. A surrogate-based multi-disciplinary design optimization framework modeling wing–propeller interaction. Aero Sci Technol 2018;78:721–33. https://doi.org/10.1016/j.ast.2018.05.002.Search in Google Scholar
13. Schatz, ME, Hermanutz, A, Baier, HJ. Multi-criteria optimization of an aircraft propeller considering manufacturing. Struct Multidiscip Optim 2017;55:899–911. https://doi.org/10.1007/s00158-016-1541-z.Search in Google Scholar
14. Li, L, Wan, H, Gao, W, Tong, F, Li, H. Reliability based multidisciplinary design optimization of cooling turbine blade considering uncertainty data statistics. Struct Multidiscip Optim 2019;59:659–73. https://doi.org/10.1007/s00158-018-2081-5.Search in Google Scholar
15. Li, Z, Lu, D, Gao, X. Optimization of mixture proportions by statistical experimental design using response surface method-A review. J Build Eng 2021;36:102101. https://doi.org/10.1016/j.jobe.2020.102101.Search in Google Scholar
16. Han, ZH, Zhang, Y, Song, CX, Zhang, KS. Weighted gradient-enhanced kriging for high-dimensional surrogate modeling and design optimization. AIAA J 2017;55:4330–46. https://doi.org/10.2514/1.j055842.Search in Google Scholar
17. Shi, R, Liu, L, Long, T, Liu, J. Sequential radial basis function using support vector machine for expensive design optimization. AIAA J 2017;55:214–27. https://doi.org/10.2514/1.j054832.Search in Google Scholar
18. Ye, W, Wang, X, Liu, Y, Chen, J. Analysis and prediction of the performance of free-piston Stirling engine using response surface methodology and artificial neural network. Appl Therm Eng 2021;188:116557. https://doi.org/10.1016/j.applthermaleng.2021.116557.Search in Google Scholar
19. Wang, Y, Yang, G, Sage, V, Xu, J, Sun, G, He, J, et al.. Optimization of dark fermentation for biohydrogen production using a hybrid artificial neural network (ANN) and response surface methodology (RSM) approach. Environ Prog Sustain Energy 2021;40:e13485. https://doi.org/10.1002/ep.13485.Search in Google Scholar
20. Ab Aziz, MF, Mostafa, SA, Foozy, CFM, Mohammed, MA, Elhoseny, M, Abualkishik, AZ. Integrating Elman recurrent neural network with particle swarm optimization algorithms for an improved hybrid training of multidisciplinary datasets. Expert Syst Appl 2021;183:115441. https://doi.org/10.1016/j.eswa.2021.115441.Search in Google Scholar
21. Renganathan, SA, Maulik, R, Ahuja, J. Enhanced data efficiency using deep neural networks and Gaussian processes for aerodynamic design optimization. Aero Sci Technol 2021;111:106522. https://doi.org/10.1016/j.ast.2021.106522.Search in Google Scholar
22. Pavese, C, Tibaldi, C, Zahle, F, Kim, T. Aeroelastic multidisciplinary design optimization of a swept wind turbine blade. Wind Energy 2017;20:1941–53. https://doi.org/10.1002/we.2131.Search in Google Scholar
23. Ceruti, A. Meta-heuristic multidisciplinary design optimization of wind turbine blades obtained from circular pipes. Eng Comput 2019;35:363–79. https://doi.org/10.1007/s00366-018-0604-8.Search in Google Scholar
24. Wang, J, P. Simacek, N. Gupta, S. Advani. Multidisciplinary tool for composite wind blade design & analysis. Compos B Eng 2018;140:91–8. https://doi.org/10.1016/j.compositesb.2017.09.075.Search in Google Scholar
25. Sederberg, TW, Parry, SR. Free-form deformation of solid geometric models. In: Proceedings of the 13th annual conference on Computer graphics and interactive techniques; 1986.10.1145/15922.15903Search in Google Scholar
26. Li, L, Jiao, J, Sun, S, Zhao, Z, Kang, J. Aerodynamic shape optimization of a single turbine stage based on parameterized free-form deformation with mapping design parameters. Energy 2019;169:444–55. https://doi.org/10.1016/j.energy.2018.12.031.Search in Google Scholar
27. Yang, F, Xu, Z. Multidisciplinary reliability analysis of turbine blade with shape uncertainty by Kriging model and free-form deformation methods. Proc Inst Mech Eng O J Risk Reliab 2020;234:611–21. https://doi.org/10.1177/1748006x19901041.Search in Google Scholar
28. Li, L, Tang, Z, Li, HH, Tong, F, Gao, W. Multidisciplinary design optimization of twin-web turbine disk with pin fins in inner cavity. Appl Therm Eng 2019;161:114104. https://doi.org/10.1016/j.applthermaleng.2019.114104.Search in Google Scholar
© 2022 Walter de Gruyter GmbH, Berlin/Boston
Articles in the same Issue
- Frontmatter
- The International Journal of Turbo and Jet Engines
- The aerothermodynamic cycle optimal design of a turbofan engine
- Multi-condition design optimization of groove flow control technique in an axial-flow pump
- Analysis on impulse characteristics of pulse detonation engine with nozzles
- Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor
- Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine
- Applicability of correlational data-mining to small-scale turbojet performance map generation
- Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application
- Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence
- Modeling and analysis of 3D radiative heat transfer in combustor
- A creep-fatigue life prediction model considering multi-factor coupling effect
- Optimization-based transient control of turbofan engines: a sequential quadratic programming approach
- Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine
- A study on design optimization for compressor blisks
- Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature
- Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor
- Predicting remaining useful life of turbofan engines using degradation signal based echo state network
- Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system
- Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage
- Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor
- Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft
- Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions
- Performance enhancement and flow separation control in an S-duct by air injection
- Gas dynamic analysis of the modern single shaft gas turbine engine flow path
- Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview
- Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils
- The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall
- Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade
- Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor
- Research on temperature rise characteristics of end V-groove ring seal
- Research on the influence of honeycomb cell blockage on the seal leakage characteristics
- Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation
- Development and application of a profile loss model considering the low-Re effect in low-pressure turbine
- Optimization of ACE mode transition control schedule considering geometric adjustment speed
- Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps
- The design method of the V-shaped groove piston ring
- Control of subsonic jets using vanes as vortex generators
- Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor
- Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed
- Effect of the distribution of the upstream probe support on performance of compressor cascade
- Effect of bypass ratio on sonic underexpanded co-flow jets with finite lip thickness
- Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter
- CFD analysis of flow control in compressor cascade using MVGs
- Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling
- Study on laser de-weight and dynamic balance technology of rotating machines
- Integrated design and analysis of inlet and missile with two side layout
- Research on turboprop engine control method based on linear parameter varying model
- Modeling and validation of the volume effect on the axial fan transient performance
- Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications
- Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties
- Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors
- Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex
- Infrared simulation of aircraft rear fuselage based on a coupled CFD method
- Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application
- Numerical study of transition process in different zones of a compressor cascade channel
Articles in the same Issue
- Frontmatter
- The International Journal of Turbo and Jet Engines
- The aerothermodynamic cycle optimal design of a turbofan engine
- Multi-condition design optimization of groove flow control technique in an axial-flow pump
- Analysis on impulse characteristics of pulse detonation engine with nozzles
- Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor
- Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine
- Applicability of correlational data-mining to small-scale turbojet performance map generation
- Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application
- Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence
- Modeling and analysis of 3D radiative heat transfer in combustor
- A creep-fatigue life prediction model considering multi-factor coupling effect
- Optimization-based transient control of turbofan engines: a sequential quadratic programming approach
- Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine
- A study on design optimization for compressor blisks
- Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature
- Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor
- Predicting remaining useful life of turbofan engines using degradation signal based echo state network
- Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system
- Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage
- Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor
- Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft
- Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions
- Performance enhancement and flow separation control in an S-duct by air injection
- Gas dynamic analysis of the modern single shaft gas turbine engine flow path
- Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview
- Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils
- The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall
- Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade
- Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor
- Research on temperature rise characteristics of end V-groove ring seal
- Research on the influence of honeycomb cell blockage on the seal leakage characteristics
- Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation
- Development and application of a profile loss model considering the low-Re effect in low-pressure turbine
- Optimization of ACE mode transition control schedule considering geometric adjustment speed
- Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps
- The design method of the V-shaped groove piston ring
- Control of subsonic jets using vanes as vortex generators
- Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor
- Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed
- Effect of the distribution of the upstream probe support on performance of compressor cascade
- Effect of bypass ratio on sonic underexpanded co-flow jets with finite lip thickness
- Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter
- CFD analysis of flow control in compressor cascade using MVGs
- Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling
- Study on laser de-weight and dynamic balance technology of rotating machines
- Integrated design and analysis of inlet and missile with two side layout
- Research on turboprop engine control method based on linear parameter varying model
- Modeling and validation of the volume effect on the axial fan transient performance
- Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications
- Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties
- Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors
- Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex
- Infrared simulation of aircraft rear fuselage based on a coupled CFD method
- Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application
- Numerical study of transition process in different zones of a compressor cascade channel
