Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors-Reference-Cited by-同舟云学术

Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors

Published:2022-06 Issue:6 Volume:60 Page:3724-3735
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bach Eric¹^ORCID,Thethy Bhavraj S.^ORCID,Edgington-Mitchell Daniel,Rezay Haghdoost Mohammad,Oliver Paschereit Christian,Stathopoulos Panagiotis,Bohon Myles D.^ORCID

Affiliation:

1. Technical University of Berlin, 10623 Berlin, Germany

Funder

Bundesministerium für Wirtschaft und Energie

Australian Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061061

Reference47 articles.

1. Recent Developments in the Research on Pressure-Gain Combustion Devices

2. An alternative architecture of the Humphrey cycle and the effect of fuel type on its efficiency

3. Effect of inlet and outlet boundary conditions on rotating detonation combustion

4. Mixing and detonation structure in a rotating detonation engine with an axial air inlet

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1. Quantitative Measurements in the Exhaust Flow of A Rotating Detonation Combustor Using Rainbow Schlieren Deflectometry;Journal of Engineering for Gas Turbines and Power;2024-08-23

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3. Continuous Injector Geometry Variation to Augment Rotating Detonation Combustor Operation and Performance;Journal of Propulsion and Power;2024-05

4. Rotating detonation combustor performance informed through a novel megahertz-rate stagnation pressure measurement;Physics of Fluids;2024-02-01

5. Rotating Detonation Combustor Performance Modeling Informed by Experimental Stagnation Pressure Measurements;AIAA SCITECH 2024 Forum;2024-01-04