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|Title:||An experimental evaluation of transient flows in a supersonic gun tunnel||Authors:||Amir, A.A.-F.
|Issue Date:||2012||Abstract:||An experimental study has been performed to investigate transient flows in a supersonic gun tunnel. The experimental work was performed using a short duration high speed flow test facility at the Universiti Tenaga Nasional (UNITEN). A physical description of the facility along with the principles of operation is provided. The pressure history of the flow process was captured using a fast response pressure transducer at three stations located at the end of the facility. Experimental measurements of shock strength, peak pressure and shock wave speed change of Air-Air as a driver/driven gas are then presented and compared with a further set of experimental measurements using the gas combination of Helium-Air. The shock wave speed was measured experimentally with a two pressure transducers technique. The results showed that the existence of the piston has a very significant influence on both the moving shock wave and peak pressure value achieved. The results provide a very good estimate for the above-mentioned parameters obtained after diaphragm rupture, and also provide a better understanding of the parameters that affect the performance of the facility. © Universiti Malaysia Pahang.||URI:||http://dspace.uniten.edu.my/jspui/handle/123456789/8539|
|Appears in Collections:||COE Scholarly Publication|
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