Effect of expansion level on the flow development with sudden expansion at high Mach numbers. (2021)

• Record Type: Journal Article
• Authors: Faheem, Mohammed; Ridwan, ; Muneer, Rayid; Aneeque, Mohammed; Afghan Khan, Sher
• Is Part Of: Materials today. Volume 46:Part 7(2021)
• Page Start: 2714
• Page End: 2725
• Publication Date: 2021
• Subjects: Sudden Expansion -- Jet State -- Supersonic Mach Numbers -- Wall Pressure -- Flow Field; Materials science -- Congresses -- Periodicals; 620.1
• DOI: 10.1016/j.matpr.2021.02.394
• Languages: English
• ISSNs: 2214-7853

Abstract

Abstract: This paper reports the experimental investigation results to monitor pressure at the base and the duct's flow development. The study aims to assess the influence of favorable and adverse pressure gradient on the flow growth and control efficacy. The experimental tests were conducted at a fixed level of favorable and unfavorable pressure gradient at the nozzles for Mach 1.25 to 3.0 at various duct lengths. Only a few selected cases are considered as representative of all the possibilities. Results show that when the nozzles are under the impact of a favorable pressure gradient, they marginally affect the duct's flow development. However, when nozzles face an adverse pressure gradient, the control acts negatively, resulting in a decline in pressure. Oscillations dominate the flow for the highest pipe length, but the flow becomes smooth for lower duct length. In most cases, flow is not negatively affected by control.