Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification
- Author
- FAN, Xiao-Qiang1 ; LI HUA1 ; JIA DI1 ; YI, Shi-He1
[1] National University of Defense Technology, ChangSha, 410073, China - Source
Journal of aircraft. 2006, Vol 43, Num 5, pp 1544-1549, 6 p ; ref : 18 ref
- CODEN
- JAIRAM
- ISSN
- 0021-8669
- Scientific domain
- Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Coin compression Couche limite Distribution pression Ecoulement transition Etude expérimentale Installation essai Interaction Modélisation Onde choc Prise air Simulation numérique Transition laminaire turbulente
- Keyword (en)
- Compression corner Boundary layers Pressure distribution Transition flow Experimental study Test facilities Interactions Modelling Shock waves Air intake Digital simulation Turbulent laminar transition
- Keyword (es)
- Chareta compresión Distribución presión Toma aire
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G27 Turbulent flows, convection, and heat transfer / 001B40G27C Transition to turbulence
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G40 Compressible flows; shock and detonation phenomena / 001B40G40N Shock-wave interactions and shock effects
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 18197707
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
10.2514/1.17040 
https://dx.doi.org/10.2514/1.17040
"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:15:\"10.2514\/1.17040\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:9:\"\u0000*\u0000jtitle\";s:19:\"Journal of aircraft\";s:9:\"\u0000*\u0000stitle\";s:8:\"J. aircr\";s:7:\"\u0000*\u0000date\";s:4:\"2006\";s:9:\"\u0000*\u0000volume\";s:2:\"43\";s:8:\"\u0000*\u0000issue\";s:1:\"5\";s:8:\"\u0000*\u0000spage\";s:4:\"1544\";s:8:\"\u0000*\u0000epage\";s:4:\"1549\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0021-8669\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:3:\"FAN\";s:10:\"\u0000*\u0000aufirst\";s:10:\"Xiao-Qiang\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:6:\"LI HUA\";i:1;s:6:\"JIA DI\";i:2;s:10:\"YI, Shi-He\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"JAIRAM\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:1:\"6\";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:15:\"10.2514\/1.17040\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:9:\"\u0000*\u0000jtitle\";s:19:\"Journal of aircraft\";s:9:\"\u0000*\u0000stitle\";s:8:\"J. aircr\";s:7:\"\u0000*\u0000date\";s:4:\"2006\";s:9:\"\u0000*\u0000volume\";s:2:\"43\";s:8:\"\u0000*\u0000issue\";s:1:\"5\";s:8:\"\u0000*\u0000spage\";s:4:\"1544\";s:8:\"\u0000*\u0000epage\";s:4:\"1549\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0021-8669\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:3:\"FAN\";s:10:\"\u0000*\u0000aufirst\";s:10:\"Xiao-Qiang\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:6:\"LI HUA\";i:1;s:6:\"JIA DI\";i:2;s:10:\"YI, Shi-He\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"JAIRAM\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:1:\"6\";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:15:\"10.2514\/1.17040\";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:15:\"10.2514\/1.17040\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:9:\"\u0000*\u0000jtitle\";s:19:\"Journal of aircraft\";s:9:\"\u0000*\u0000stitle\";s:8:\"J. aircr\";s:7:\"\u0000*\u0000date\";s:4:\"2006\";s:9:\"\u0000*\u0000volume\";s:2:\"43\";s:8:\"\u0000*\u0000issue\";s:1:\"5\";s:8:\"\u0000*\u0000spage\";s:4:\"1544\";s:8:\"\u0000*\u0000epage\";s:4:\"1549\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0021-8669\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:3:\"FAN\";s:10:\"\u0000*\u0000aufirst\";s:10:\"Xiao-Qiang\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:6:\"LI HUA\";i:1;s:6:\"JIA DI\";i:2;s:10:\"YI, Shi-He\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"JAIRAM\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:1:\"6\";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:15:\"10.2514\/1.17040\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:9:\"\u0000*\u0000jtitle\";s:19:\"Journal of aircraft\";s:9:\"\u0000*\u0000stitle\";s:8:\"J. aircr\";s:7:\"\u0000*\u0000date\";s:4:\"2006\";s:9:\"\u0000*\u0000volume\";s:2:\"43\";s:8:\"\u0000*\u0000issue\";s:1:\"5\";s:8:\"\u0000*\u0000spage\";s:4:\"1544\";s:8:\"\u0000*\u0000epage\";s:4:\"1549\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0021-8669\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:3:\"FAN\";s:10:\"\u0000*\u0000aufirst\";s:10:\"Xiao-Qiang\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:6:\"LI HUA\";i:1;s:6:\"JIA DI\";i:2;s:10:\"YI, Shi-He\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"JAIRAM\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:1:\"6\";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:15:\"10.2514\/1.17040\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:9:\"\u0000*\u0000jtitle\";s:19:\"Journal of aircraft\";s:9:\"\u0000*\u0000stitle\";s:8:\"J. aircr\";s:7:\"\u0000*\u0000date\";s:4:\"2006\";s:9:\"\u0000*\u0000volume\";s:2:\"43\";s:8:\"\u0000*\u0000issue\";s:1:\"5\";s:8:\"\u0000*\u0000spage\";s:4:\"1544\";s:8:\"\u0000*\u0000epage\";s:4:\"1549\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:9:\"0021-8669\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:3:\"FAN\";s:10:\"\u0000*\u0000aufirst\";s:10:\"Xiao-Qiang\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:6:\"LI HUA\";i:1;s:6:\"JIA DI\";i:2;s:10:\"YI, Shi-He\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:0:\"\";s:8:\"\u0000*\u0000coden\";s:6:\"JAIRAM\";s:8:\"\u0000*\u0000genre\";s:7:\"article\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:0:\"\";s:8:\"\u0000*\u0000title\";s:111:\"Experimental investigation on forced boundary-layer transition of axisymmetric inlet and numerical verification\";s:8:\"\u0000*\u0000place\";s:10:\"Reston, VA\";s:6:\"\u0000*\u0000pub\";s:50:\"American Institute of Aeronautics and Astronautics\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:1:\"6\";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
