Oblique Detonation Wave Control with O<sub>3</sub> and H<sub>2</sub>O<sub>2</sub> Sensitization in Hypersonic Flow

Oblique Detonation Wave Control with O<sub>3</sub> and H<sub>2</sub>O<sub>2</sub> Sensitization in Hypersonic Flow

This numerical study investigates the effects of adding a small amount of ignition promoters for controlling the wedge-induced oblique shock wave (OSW) to oblique detonation wave (ODW) transition in a premixed hydrogen–air mixture at hypersonic speeds. The time-dependent two-dimensional compressible...

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Bibliographic Details
Main Authors: Ashish Vashishtha, Snehasish Panigrahy, Dino Campi, Dean Callaghan, Cathal Nolan, Ralf Deiterding
Format: Article
Language:English
Published: MDPI AG 2022-06-01
Series:Energies
Subjects:
schramjet
oblique detonation wave
hypersonic flow
detailed chemical kinetics
fuel-sensitization
Online Access:https://www.mdpi.com/1996-1073/15/11/4140

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https://www.mdpi.com/1996-1073/15/11/4140

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