Estimation of Characteristic Data of Aircraft Engine Compressor based on Developed Modeling Method
-
Zeng Li
and
Long Wei
Abstract
To resolve the problem of low estimation accuracy of compressor characteristic parameters based on traditional Kriging model, an improved interpolation method of aircraft engine compressor characteristic parameters based on the Kriging algorithm is proposed. Considering the distribution feature of original data, a high dimensional model is built. By defining the relationship between input and output data, an unknown vector composed of characteristic parameters at a certain speed of
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Articles in the same Issue
- Frontmatter
- Estimation of Characteristic Data of Aircraft Engine Compressor based on Developed Modeling Method
- Conjugate Heat Transfer Analysis on the Interior Surface of Nozzle Guide Vane with Combined Impingement and Film Cooling
- Prediction of Lean Blowout Limits for Methane-Air Bluff Body Stabilized Combustion using a Temperature Gradient Method in a Model Gas-Turbine Afterburner
- Investigation of Film Cooling Effectiveness of Dual-fanned Hole with Various Exit Widths
- Performance Seeking Control of Propfan Engines Based on Modified Cuckoo Search
- A New Scheduling Method for TTCAN-Based Turbofan Distributed Control System
- Numerical Investigation of Three-dimensional Separation Control on a High-speed Compressor Stator Vane with Tailored Synthetic Jet
- Aerodynamic Optimization of Winglet-Cavity Tip in an Axial High Pressure Turbine Stage
- Estimation of Gas Turbine Unmeasured Variables for an Online Monitoring System
Articles in the same Issue
- Frontmatter
- Estimation of Characteristic Data of Aircraft Engine Compressor based on Developed Modeling Method
- Conjugate Heat Transfer Analysis on the Interior Surface of Nozzle Guide Vane with Combined Impingement and Film Cooling
- Prediction of Lean Blowout Limits for Methane-Air Bluff Body Stabilized Combustion using a Temperature Gradient Method in a Model Gas-Turbine Afterburner
- Investigation of Film Cooling Effectiveness of Dual-fanned Hole with Various Exit Widths
- Performance Seeking Control of Propfan Engines Based on Modified Cuckoo Search
- A New Scheduling Method for TTCAN-Based Turbofan Distributed Control System
- Numerical Investigation of Three-dimensional Separation Control on a High-speed Compressor Stator Vane with Tailored Synthetic Jet
- Aerodynamic Optimization of Winglet-Cavity Tip in an Axial High Pressure Turbine Stage
- Estimation of Gas Turbine Unmeasured Variables for an Online Monitoring System
