A numerical prediction and flight test of the transient fuel temperatures in an aircraft
- Author
- YEONG JUN KIM1 ; CHANG NYUNG KIM2 3
[1] Korea Aerospace Industries, Kyung Hee University, Korea, Republic of
[2] College of Advance Technology, Kyung Hee University, Korea, Republic of
[3] Industrial Liaison Research Institute, Kyung Hee University, Korea, Republic of - Source
Journal of mechanical science and technology. 2007, Vol 21, Num 12, pp 2250-2260, 11 p ; ref : 12 ref
- ISSN
- 1738-494X
- Scientific domain
- Mechanics acoustics
- Publisher
- Korean Society of Mechanical Engineers, Seoul
- Publication country
- Korea, Republic of
- Document type
- Article
- Language
- English
- Author keyword
- Additional fuel supplies Aircraft fuel system Flight test Fuel Thermal Management System (FTMS) Fuel temperature
- Keyword (fr)
- Alimentation combustible Aéronef Carburéacteur Combustible Comportement thermique Conservation énergie Convection Différence température Ecoulement libre Ecoulement turbulent Fonction courant Loi conservation Modélisation Méthode différence finie Méthode empirique Plaque plane Réponse transitoire Transfert chaleur Vol
- Keyword (en)
- Fuel feed Aircraft Jet engine fuels Fuels Thermal behavior Energy conservation Convection Temperature difference Free flow Turbulent flow Stream function Conservation laws Modelling Finite difference method Empirical method Flat plate Transient response Heat transfer Theft
- Keyword (es)
- Alimentación combustible Comportamiento térmico Diferencia temperatura Flujo libre Función corriente Método empírico Placa plana
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40D Heat transfer / 001B40D05 Analytical and numerical techniques
- Discipline
- Physics : heat transfer
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 19912717
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Access to the document
Install on your browser
DOI
10.1007/BF03177487 
https://dx.doi.org/10.1007/BF03177487
"O:13:\"PanistOpenUrl\":36:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000idc\";N;s:6:\"\u0000*\u0000fmt\";s:7:\"journal\";s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:9:\"\u0000*\u0000jtitle\";s:44:\"Journal of mechanical science and technology\";s:9:\"\u0000*\u0000stitle\";s:21:\"J. Mech. Sci. Technol\";s:7:\"\u0000*\u0000date\";s:4:\"2007\";s:9:\"\u0000*\u0000volume\";s:2:\"21\";s:8:\"\u0000*\u0000issue\";s:2:\"12\";s:8:\"\u0000*\u0000spage\";s:4:\"2250\";s:8:\"\u0000*\u0000epage\";s:4:\"2260\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"1738-494X\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:13:\"YEONG JUN KIM\";s:10:\"\u0000*\u0000aufirst\";s:0:\"\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:15:\"CHANG NYUNG KIM\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:8:\"\u0000*\u0000place\";s:5:\"Seoul\";s:6:\"\u0000*\u0000pub\";s:38:\"Korean Society of Mechanical Engineers\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"11\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Panist access
"O:12:\"IstexOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:7:\"journal\";s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:9:\"\u0000*\u0000jtitle\";s:44:\"Journal of mechanical science and technology\";s:9:\"\u0000*\u0000stitle\";s:21:\"J. Mech. Sci. Technol\";s:7:\"\u0000*\u0000date\";s:4:\"2007\";s:9:\"\u0000*\u0000volume\";s:2:\"21\";s:8:\"\u0000*\u0000issue\";s:2:\"12\";s:8:\"\u0000*\u0000spage\";s:4:\"2250\";s:8:\"\u0000*\u0000epage\";s:4:\"2260\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"1738-494X\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:13:\"YEONG JUN KIM\";s:10:\"\u0000*\u0000aufirst\";s:0:\"\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:15:\"CHANG NYUNG KIM\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:8:\"\u0000*\u0000place\";s:5:\"Seoul\";s:6:\"\u0000*\u0000pub\";s:38:\"Korean Society of Mechanical Engineers\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"11\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Istex access
"O:16:\"UnpaywallOpenUrl\":35:{s:8:\"\u0000*\u0000email\";s:27:\"assistance-portail@inist.fr\";s:6:\"\u0000*\u0000fmt\";N;s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";N;s:7:\"\u0000*\u0000pmid\";N;s:9:\"\u0000*\u0000atitle\";N;s:9:\"\u0000*\u0000jtitle\";N;s:9:\"\u0000*\u0000stitle\";N;s:7:\"\u0000*\u0000date\";N;s:9:\"\u0000*\u0000volume\";N;s:8:\"\u0000*\u0000issue\";N;s:8:\"\u0000*\u0000spage\";N;s:8:\"\u0000*\u0000epage\";N;s:8:\"\u0000*\u0000pages\";N;s:7:\"\u0000*\u0000issn\";N;s:8:\"\u0000*\u0000eissn\";N;s:9:\"\u0000*\u0000aulast\";N;s:10:\"\u0000*\u0000aufirst\";N;s:9:\"\u0000*\u0000auinit\";N;s:10:\"\u0000*\u0000auinitm\";N;s:5:\"\u0000*\u0000au\";N;s:9:\"\u0000*\u0000aucorp\";N;s:7:\"\u0000*\u0000isbn\";N;s:8:\"\u0000*\u0000coden\";N;s:8:\"\u0000*\u0000genre\";N;s:7:\"\u0000*\u0000part\";N;s:9:\"\u0000*\u0000btitle\";N;s:8:\"\u0000*\u0000title\";N;s:8:\"\u0000*\u0000place\";N;s:6:\"\u0000*\u0000pub\";N;s:10:\"\u0000*\u0000edition\";N;s:9:\"\u0000*\u0000tpages\";N;s:9:\"\u0000*\u0000series\";N;s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";N;}"
Unpaywall access
"O:16:\"EuropePMCOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:7:\"journal\";s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:9:\"\u0000*\u0000jtitle\";s:44:\"Journal of mechanical science and technology\";s:9:\"\u0000*\u0000stitle\";s:21:\"J. Mech. Sci. Technol\";s:7:\"\u0000*\u0000date\";s:4:\"2007\";s:9:\"\u0000*\u0000volume\";s:2:\"21\";s:8:\"\u0000*\u0000issue\";s:2:\"12\";s:8:\"\u0000*\u0000spage\";s:4:\"2250\";s:8:\"\u0000*\u0000epage\";s:4:\"2260\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"1738-494X\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:13:\"YEONG JUN KIM\";s:10:\"\u0000*\u0000aufirst\";s:0:\"\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:15:\"CHANG NYUNG KIM\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:8:\"\u0000*\u0000place\";s:5:\"Seoul\";s:6:\"\u0000*\u0000pub\";s:38:\"Korean Society of Mechanical Engineers\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"11\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Europe PubMed Central access
"O:11:\"BaseOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:7:\"journal\";s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:9:\"\u0000*\u0000jtitle\";s:44:\"Journal of mechanical science and technology\";s:9:\"\u0000*\u0000stitle\";s:21:\"J. Mech. Sci. Technol\";s:7:\"\u0000*\u0000date\";s:4:\"2007\";s:9:\"\u0000*\u0000volume\";s:2:\"21\";s:8:\"\u0000*\u0000issue\";s:2:\"12\";s:8:\"\u0000*\u0000spage\";s:4:\"2250\";s:8:\"\u0000*\u0000epage\";s:4:\"2260\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"1738-494X\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:13:\"YEONG JUN KIM\";s:10:\"\u0000*\u0000aufirst\";s:0:\"\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:15:\"CHANG NYUNG KIM\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:8:\"\u0000*\u0000place\";s:5:\"Seoul\";s:6:\"\u0000*\u0000pub\";s:38:\"Korean Society of Mechanical Engineers\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"11\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Base Search access
"O:12:\"ArXivOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:7:\"journal\";s:6:\"\u0000*\u0000doi\";s:18:\"10.1007\/BF03177487\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:9:\"\u0000*\u0000jtitle\";s:44:\"Journal of mechanical science and technology\";s:9:\"\u0000*\u0000stitle\";s:21:\"J. Mech. Sci. Technol\";s:7:\"\u0000*\u0000date\";s:4:\"2007\";s:9:\"\u0000*\u0000volume\";s:2:\"21\";s:8:\"\u0000*\u0000issue\";s:2:\"12\";s:8:\"\u0000*\u0000spage\";s:4:\"2250\";s:8:\"\u0000*\u0000epage\";s:4:\"2260\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"1738-494X\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:13:\"YEONG JUN KIM\";s:10:\"\u0000*\u0000aufirst\";s:0:\"\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:1:{i:0;s:15:\"CHANG NYUNG KIM\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:88:\"A numerical prediction and flight test of the transient fuel temperatures in an aircraft\";s:8:\"\u0000*\u0000place\";s:5:\"Seoul\";s:6:\"\u0000*\u0000pub\";s:38:\"Korean Society of Mechanical Engineers\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:2:\"11\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
arXiv access
