Sonic injection through diamond orifices into a hypersonic flow.

摘要

The objective for the present study was to experimentally characterize the performance of diamond shaped injectors for hypersonic flow applications. First, an extensive literature review was performed. Second, a small scale Mach 5.0 wind tunnel facility was installed. Third, a detailed experimental parametric investigation of sonic injection through a diamond orifice (five incidence angles and three momentum ratios) and a circular injector (three momentum ratios) into the Mach 5.0 freestream was performed. Also, the use of downstream plume vorticity control ramps was investigated. Fourth, a detailed analysis of the experimental data to characterize and model the flow for the present range of conditions was achieved. The experimental techniques include surface oil flow visualization, Mie-Scattering flow visualization, particle image velocimetry (PIV), shadowgraph photograph, and a five-hole mean flow probe.; The results show that the diamond injectors have the potential to produce attached shock depending on the incidence angle and jet momentum ratio. For example, the incidence angles less than or equal to 45° at J = 0.43 generated attached interaction shocks. The attached shock produced reduced total pressure loss (drag for scramjet) and eliminated potential hot spots, associated with the upstream flow separation. The jet interaction shock angle increased with jet incidence angle and momentum ratio due to increased penetration and flow disturbances. The plume penetration and cross-sectional area increased with incidence angle and momentum ratio. The increased jet interaction shock angle and strength produced increased total pressure loss, jet interaction force and total normal force. The characteristic kidney bean shaped plume was not discernable from the diamond injectors indicating increased effectiveness for film cooling applications. A vorticity generation ramp increased the penetration of the plume and the plume shape was indicative of higher levels of vorticity.; In conclusion, first, this study provided a full characterization of the mean flow physics for diamond injection into a hypersonic cross flow. Second, a detailed analysis of the experimental data resulted in new understanding and models for the presently studied flow conditions. Third, this research project resulted in a new hypersonic wind tunnel and instrumentation apparatus.