Experimental investigations on the power extraction of a turbine driven by a pulse detonation combustor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference21 articles.
1. Propulsive performance of air breathing pulse detonation engines;Ma;J Propul Power,2006
2. Pulse detonation engine as a ramjet replacement;Harris;J Propul Power,2006
3. Thermodynamic cycle analysis of pulse detonation engines;Heiser;J Propul Power,2002
4. Thermodynamics of air breathing pulse-detonation engines;Kentfield;J Propul Power,2002
5. System-level performance estimation of a pulse detonation based hybrid engine;Goldmeer;J Eng Gas Turbines Power,2008
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1. Reheat effect on the improvement in efficiency of the turbine driven by pulse detonation;Defence Technology;2024-01
2. Effect of back-propagation pressure on axial flow compressor in a pulse detonation turbine engine;Aerospace Science and Technology;2023-10
3. Effects of detonation initial conditions on performance of pulse detonation chamber-axial turbine combined system;Energy;2023-09
4. Experimental Investigations on Detonation Initiation Characteristics of a Liquid-Fueled Pulse Detonation Combustor at Different Inlet Air Temperatures;Energies;2022-12-01
5. Analysis of Dynamic Operating Characteristics of a Pulse Detonation Turbine Engine;Aerospace;2022-09-26
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