The invention discloses a
compression system end area flow regulation and control method based on blade inner cooling under a low Reynolds number. Firstly, through calculation or measurement, a
compression system end area three-dimensional flow field under different Reynolds numbers is obtained, and the end area loss variation degree is quantified. Then, revealing regulation and control rules of different isothermal cooling wall
surface conditions on near-wall fluid
physical property parameters, boundary layer growth rate and end region secondary flow migration intensity under a low Reynolds number, and establishing a correlation model of end region loss reduction and efficiency improvement and wall
surface cooling intensity; and on the basis, a blade built-in
convection cooling channel structure is designed, the
cooling channel and blade surface flow heat characteristics are analyzed based on a conjugate
heat transfer method, and inner
cooling channel structure parameters are optimized until the wall surface
temperature drop amplitude meets the preset requirement. And finally, checking the wall
surface cooling effect, and measuring end region performance parameters during inner cooling regulation and control under a low Reynolds number to complete scheme
verification. By introducing blade inner cooling, the flow characteristic of an end region can be remarkably improved on the premise that the structural complexity is not increased as much as possible, and stable and efficient operation of a
compression system under the low Reynolds number is guaranteed.