Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements
In: International Journal of Aeronautical and Space Sciences, 2024-04-22, S. 1-21
Online
academicJournal
Zugriff:
Titel: |
Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements
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Autor/in / Beteiligte Person: | Kim, Young Jin ; Lee, Hyoung Jin ; Lee, Bok Jik |
Link: | |
Zeitschrift: | International Journal of Aeronautical and Space Sciences, 2024-04-22, S. 1-21 |
Veröffentlichung: | 2024 |
Medientyp: | academicJournal |
ISSN: | 2093-274X (print) ; 2093-2480 (print) |
DOI: | 10.1007/s42405-024-00725-5 |
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