An empirical model for stagnation pressure gain in rotating detonation combustors

Author:

Bach EricORCID,Paschereit C.O.,Stathopoulos Panagiotis,Bohon Myles D.ORCID

Funder

Bundesministerium für Wirtschaft und Energie

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference15 articles.

1. Continuous spin detonations;Bykovskii;J. Propul. Power,2006

2. D. A. Schwer, C. M. Brophy, R. H. Kelso, Pressure characteristics of an aerospike nozzle in a rotating detonation engine, AIAA Paper 2018–4968, July 2018.

3. High-speed diagnostics in a natural GasAir rotating detonation engine;Journell;J. Propul. Power,2020

4. Demonstrated low loss and low equivalence ratio operation of a rotating detonation engine for power generation;Stout,2020

5. Determining the pressure gain of pressure gain combustion;Kaemming,2018

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