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Numerical Investigation of a Nested Double Annular Combustion Chamber Configuration for Rotating Detonation Engine Applications Cover

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Numerical Investigation of a Nested Double Annular Combustion Chamber Configuration for Rotating Detonation Engine Applications

Transactions on Aerospace Research

Volume 2026 (2026): Issue 1 (March 2026)

By: Rin Okada , Edyta Dzieminska , Michał Kawalec and Wenjing Cao

Open Access

|Mar 2026

Figures & tables

Authors

Rin Okada

Sophia University, Faculty of Science and Technology, Chiyoda-ku, Tokyo, Japan

Edyta Dzieminska

edyta.d@sophia.ac.jp

Sophia University, Faculty of Science and Technology, Chiyoda-ku, Tokyo, Japan

Michał Kawalec

Łukasiewicz Research Network - Institute of Aviation, Warsaw, Poland

Wenjing Cao

Sophia University, Faculty of Science and Technology, Chiyoda-ku, Tokyo, Japan

Articles in this issue

DOI: https://doi.org/10.2478/tar-2026-0005 | Journal eISSN: 2545-2835

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Language: English

Page range: 107 - 120

Submitted on: May 30, 2025

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Accepted on: Feb 6, 2026

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Published on: Mar 18, 2026

Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION

In partnership with: Paradigm Publishing Services

Publication frequency: 4 issues per year

Keywords:

Rotating Detonation Engine (RDE),

supersonic combustion,

computational fluid dynamics (CFD),

double-chamber design,

propulsion efficiency,

thrust optimization,

Related subjects:

Introductions and overviews,

Engineering, other,

Geosciences, other,

Materials sciences,

Materials sciences, other,

© 2026 Rin Okada, Edyta Dzieminska, Michał Kawalec, Wenjing Cao, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.

Volume 2026 (2026): Issue 1 (March 2026)

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