学术文献库

A geometrical mechanism that generates augmented swirling and round jets is being proposed. The proposed geometry has an axial inlet port and three tangential inlet ports, each of diameter 10mm. A parameter called Split ratio, defined as the percentage of airflow split through these inlet ports, is introduced for the augmented jet. Flow at four different split ratios(SR 1,2,3, and 4) results in a single augmented jet of swirling and round jets of diameter D = 30mm, for which impingement heat transfer is predicted using 3D RANS numerical simulations. Also, computations for conventional round jets and swirling jets generated by an in-house geometrical vane swirler of 45, 60 and 30 degree vane angles each of jet diameter D = 30 mm are performed for the Reynolds number (Re = 6000 to 15,000) and at a jet-plate distance (H = 1.5D to 4D). A comparative study of the flow structures for all the jets using computations is done, followed by a limited discussion on Particle Image velocimetry (PIV) flow visualization results. An impingement heat transfer analysis for all the jets is studied numerically. It is inferred that at a smaller jet-plate distance H =1.5D, the augmented jet and vane swirler jets showed an improved heat transfer from the impingement surface (heated flat plate). In contrast, the conventional round jets showed maximum heat transfer at H = 4D. From the comparative study, the impingement heat transfer characteristics using the proposed augmented jet are better at an optimized jet-plate distance H=1.5D and at a split ratio (SR 4), with an enhancement in the average Nusselt number (Nu avg) of 88% than the conventional round jet and 101% than the vane-swirler jet counterpart. Similarly, an enhancement in the stagnation Nusselt number (Nu stg) of 189% than the round jet is predicted for the proposed augmented jet at SR-4.