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Title: Reduced-order-modeling of the transient starting in supersonic passages

Journal Article · · Aerospace Science and Technology

Not Available

Research Organization:
Purdue University, West Lafayette, IN (United States)
Sponsoring Organization:
European Union (EU); USDOE
OSTI ID:
1983381
Journal Information:
Aerospace Science and Technology, Journal Name: Aerospace Science and Technology Journal Issue: C Vol. 139; ISSN 1270-9638
Publisher:
ElsevierCopyright Statement
Country of Publication:
France
Language:
English

References (29)

Effects of supersonic nozzle guide vanes on the performance and flow structures of a rotating detonation combustor journal April 2022
Investigation of hypersonic inlet pulse-starting characteristics at high Mach number journal November 2016
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers journal March 2018
Starting characteristics and phenomenon of a supersonic wind tunnel coupled with inlet model journal June 2018
Numerical investigation on the assistant restarting method of variable geometry for high Mach number inlet journal August 2018
Performance analysis of dual-duct rotating detonation aero-turbine engine journal September 2019
Prediction of self-starting limit of two-dimensional supersonic inlets considering viscous effects journal November 2020
Feasibility of employing the restarting process to evaluate the self-starting ability for hypersonic inlets journal December 2020
Experimental investigation on detonation wave propagation mode in the start-up process of rotating detonation turbine engine journal April 2021
Experimental investigation of start/unstart process during hypersonic intake at Mach 6 and its control journal June 2021
Buzz characteristics and separation bubble dynamics in supersonic intake journal August 2021
Analysis of energy saving and thrust characteristics of rotating detonation turbine engine journal May 2022
A real-time online unstart prediction approach for supersonic inlet journal November 2022
Numerical study of unsteady starting characteristics of a hypersonic inlet journal June 2013
Performance analysis of a rotating detonation combustor based on stagnation pressure measurements journal July 2020
Aerodynamic response of internal passages to pulsating inlet supersonic conditions journal June 2017
Design and analysis of pioneering high supersonic axial turbines journal December 2014
On the transient response of the turbulent boundary layer inception in compressible flows journal July 2018
Response of a turbulent boundary layer to rapid freestream acceleration journal April 2020
Characterization of a Supersonic Turbine Downstream of a Rotating Detonation Combustor journal October 2018
Experimental Investigations of the Performance and Unsteady Behaviour of a Supersonic Intake journal May 2007
Limiting Contractions for Starting Simple Ramp-Type Scramjet Intakes with Overboard Spillage journal September 2008
Unsteady Strong Shock Interactions in a Transonic Turbine: Experimental and Numerical Analysis journal July 2008
Inlet Starting of High-Contraction Axisymmetric Scramjets journal November 2010
Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets journal March 2016
Modified Kantrowitz Starting Criteria for Mixed Compression Supersonic Intakes journal May 2019
Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors journal June 2022
Entropy Minimization Design Approach of Supersonic Internal Passages journal August 2015
Descending Modal Transition Dynamics in a Large Eddy Simulation of a Rotating Detonation Rocket Engine journal June 2021

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