Experimental Studies on Shock Boundary Layer Interactions using Micro-Ramps at Mach 5

  • Mohd Saad

Student thesis: Phd

Abstract

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Date of Award31 Dec 2014
Original languageEnglish
Awarding Institution
  • The University of Manchester
SupervisorKonstantinos Kontis (Supervisor)

Keywords

  • shock boundary layer interactions
  • micro-ramp
  • micro vortex generator
  • hypersonic flow control

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