The invention discloses a
polynomial chaos-based
turbine blade tip gas thermal performance
uncertainty quantification system. The
system comprises a parameterized
geometric modeling module, a sampling point generation module, a
polynomial chaos expansion model construction module, a sample point initial field distribution module, a
turbine blade tip gas heat performance full-automatic pretreatment module, a multi-core remote asynchronous distributed calculation module, a calculation progress real-time feedback module, a
polynomial chaos expansion coefficient solving module, a
sensitivity analysis module, a result file sampling and analysis module and the like. According to the
turbine blade tip gas thermal performance uncertainty detection
system, the number of samples needed for obtaining the
turbine blade tip gas thermal performance uncertainty can be greatly reduced, the time needed for calculating the numerical value of a
single sample can be shortened, and the system is further suitable for
turbine blade tips of any size and form; and the requirements of designers of the turbine cooling system are better met.