Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
EFFECTS OF THE REACTION MECHANISM ON HEAT RELEASE FOR THE PREDICTION OF THERMOACOUSTIC INSTABILITIES IN LIQUID ROCKET ENGINES
Date
2023-09-13
Author
Öztürkmen, Musa Onur
Özyörük, Yusuf
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
35
views
0
downloads
Cite This
URI
http://aiac.ae.metu.edu.tr/
https://hdl.handle.net/11511/106695
Conference Name
12th Ankara International Aerospace Conference
Collections
Department of Aerospace Engineering, Conference / Seminar
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
M. O. Öztürkmen and Y. Özyörük, “EFFECTS OF THE REACTION MECHANISM ON HEAT RELEASE FOR THE PREDICTION OF THERMOACOUSTIC INSTABILITIES IN LIQUID ROCKET ENGINES,” presented at the 12th Ankara International Aerospace Conference, Ankara, Türkiye, 2023, Accessed: 00, 2023. [Online]. Available: http://aiac.ae.metu.edu.tr/.
