Différences

Ci-dessous, les différences entre deux révisions de la page.

--- public:modeles:rotor_38:accueil [2023/03/28 11:25] – solenekojtych
+++ public:modeles:rotor_38:accueil [2023/04/05 09:04] (Version actuelle) – modification externe 127.0.0.1
@@ Ligne 13: / Ligne 13: @@
 ===== About =====
-Rotor 38 is part of a research program to study a advanced-core compressor design with a high compression ratio (20:1). It is therefore the fourth stage rotor of this eight stage transonic compressor. Of these eight stages, the first four have been designed and tested : rotors 35, 36, 37 and 38. For more information, here is a link to [[https://ntrs.nasa.gov/citations/19780025165|report from NASA]].
+Rotor 38 is part of a research program to study a advanced-core compressor design with a high compression ratio (20:1). It is therefore the fourth stage rotor of this eight stage transonic compressor. Of these eight stages, the first four have been designed and tested : rotors 35, 36, 37 and 38. For more information, here is a link to [[https://ntrs.nasa.gov/citations/19780025165|a report from NASA]].
   * Original technical report [(cite:moore1982design>Moore R.D., Reid L. «Performance of Single-Stage Axial-Flow Transonic Compressor With Rotor and Stator Aspect Ratios of 1.63 and 1.77, Respectively, and With Design Pressure Ratio of 2.05 » 1982.  {{ https://ntrs.nasa.gov/citations/19820014395|pdf}})]: <code>@TechReport{moore1982design,
@@ Ligne 27: / Ligne 27: @@
   * Picture :
 {{ :public:modeles:rotor_38:gene_aubes_nasa_image_rotor38.png?300 |}}
-<caption>Fig1. https://catalog.archives.gov/id/17466806 </caption>
+<caption>Fig. 1 https://catalog.archives.gov/id/17466806 </caption>
-<code>@Misc{brown1977records,
+  * <code>@Misc{brown1977records,
 author   = {Brown, M.},
 title    = {Rotor 35 - Rotor 38 - Stator 35 in casing. {R}ecords of the {N}ational {A}eronautics and {S}pace {A}dministration, 1903 - 2006. {P}hotographs relating to agency activities, facilities and personnel, 1973 - 2013},
-note     = {\href{https://catalog.archives.gov/id/17466806}{https://catalog.archives.gov/id/17466806}, 1977 }, % for Fig. 1}
+year     = {1977},
+url     = {https://catalog.archives.gov/id/17466806}}
 </code>
@@ Ligne 145: / Ligne 146: @@
 ===== À propos =====
-Le rotor 38 appartient à un programme de recherche visant à étudier une conception de compresseur possédant un grand taux de compression (20:1). Il est donc le rotor du quatrième étage de ce compresseur transsonique de huit étages. Parmi ces huit étages, les quatre premiers ont été conçus et testés, ils correspondent aux rotors 35, 36, 37 et 38. Pour plus d'information, voici un lien vers [[https://ntrs.nasa.gov/citations/19780025165|rapport de la NASA]].
+Le rotor 38 appartient à un programme de recherche visant à étudier une conception de compresseur possédant un grand taux de compression (20:1). Il est donc le rotor du quatrième étage de ce compresseur transsonique de huit étages. Parmi ces huit étages, les quatre premiers ont été conçus et testés, ils correspondent aux rotors 35, 36, 37 et 38. Pour plus d'information, voici un lien vers [[https://ntrs.nasa.gov/citations/19780025165|un rapport de la NASA]].
   * Rapport technique original[(cite:moore1982design>)]: <code>@TechReport{moore1982design,
@@ Ligne 159: / Ligne 160: @@
 {{ :public:modeles:rotor_38:gene_aubes_nasa_image_rotor38.png?300 |}}
 <caption>Fig1. https://catalog.archives.gov/id/17466806 </caption>
-<code>@Misc{brown1977records,
+  * <code>@Misc{brown1977records,
 author   = {Brown, M.},
 title    = {Rotor 35 - Rotor 38 - Stator 35 in casing. {R}ecords of the {N}ational {A}eronautics and {S}pace {A}dministration, 1903 - 2006. {P}hotographs relating to agency activities, facilities and personnel, 1973 - 2013},
-note     = {\href{https://catalog.archives.gov/id/17466806}{https://catalog.archives.gov/id/17466806}, 1977 }, % for Fig. 1}
+year     = {1977},
+url     = {https://catalog.archives.gov/id/17466806}}
 </code>