Authors
Institute of Fluid-Flow Machinery, Polish Academy of Sciences, Gdansk, Poland
Test Section Design for Measuring the Drag Coefficient of a Suborbital Rocket Model at Ma 2.45
DOI: https://doi.org/10.2478/tar-2024-0018 | Journal eISSN: 2545-2835
Language: English
Page range: 86 - 100
Submitted on: May 20, 2024
Accepted on: Jul 12, 2024
Published on: Sep 11, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
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© 2024 Filip Wasilczuk, Marcin Kurowski, Paweł Flaszyński, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.