Title
Advances On The Stabilization Of Standing Continuous Detonation For Pressure Gain Propulsion
Abstract
This work outlines the recent advancements of a hypersonic combustor to study the stabilization of normal and oblique detonation waves. The current high-enthalpy combustor provides a Mach 5 flow for the study of oblique detonation wave stabilization utilizing air and hydrogen. Recent results in the advances of high pressure burning capabilities, nozzle inlet temperature measurements and supersonic flow verification via Mach wave angle measurements from Schlieren imaging are presented.
Publication Date
1-1-2017
Publication Title
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
DOI Link
https://doi.org/10.2514/6.2017-4909
Copyright Status
Unknown
Socpus ID
85085850586 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/85085850586
STARS Citation
Sosa, Jonathan; Hoban, Matthew; and Ahmed, Kareem A., "Advances On The Stabilization Of Standing Continuous Detonation For Pressure Gain Propulsion" (2017). Scopus Export 2015-2019. 6711.
https://stars.library.ucf.edu/scopus2015/6711