Différences

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

--- public:modeles:rotor_35:accueil [2023/03/28 11:06] – solenekojtych
+++ public:modeles:rotor_35:accueil [2023/04/15 13:29] (Version actuelle) – [Material properties] ikrambeghdadi
@@ Ligne 13: / Ligne 13: @@
 ===== Original model =====
-Rotor 35 is part of a research program to study a advanced-core compressor design with a high compression ratio (20:1). It is therefore the first 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 35 is part of a research program to study a advanced-core compressor design with a high compression ratio (20:1). It is therefore the first 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:reid1978performance>Reid L., Moore R. D. «Performance of Single-Stage Axial-Flow Transonic Compressor With Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio of 1.82 » 1978.  {{ https://ntrs.nasa.gov/citations/19790001889|pdf}})]:
@@ Ligne 27: / Ligne 27: @@
   * Picture :
 {{ :public:modeles:rotor_35:gene_aubes_nasa_image_rotor35.png?300 |}}
-<caption>Fig1. https://catalog.archives.gov/id/17466807 </caption>
+<caption>Fig. 1 https://catalog.archives.gov/id/17466807 </caption>
    * <code>@Misc{brown1977records,
 author   = {Brown, M.},
@@ Ligne 62: / Ligne 62: @@
 ===== Material properties  =====
-Rotor 35 is made of a 200-grade maraging steel[(cite:reid1978designandoverall>Reid //et all//. «Design and overall performance of four highly loaded, high-speed inlet stages for and advanced high-pressure-ratio core compressor» 1978.  {{ https://ntrs.nasa.gov/citations/19780025165|pdf}})], but the exact material properties are not provided in the NASA report. The following properties are considered:
+Rotor 35 is made of a 200-grade maraging steel[(cite:reid1978designandoverall>Reid //et all//. «Design and overall performance of four highly loaded, high-speed inlet stages for and advanced high-pressure-ratio core compressor» 1978.  {{ https://ntrs.nasa.gov/citations/19780025165|pdf}})], but the exact material properties are not provided in the NASA report. The following properties are considered :
-Considered properties: 18-Ni-200-maraging steel :
 ^                         ^  unité    ^ valeurs             ^
@@ Ligne 144: / Ligne 142: @@
 ===== Modèle original =====
-Le rotor 35 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 premier 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 35 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 premier 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:reid1978design>)]: <code>@TechReport{reid1982design,
@@ Ligne 157: / Ligne 155: @@
   * Photographie :
 {{ :public:modeles:rotor_35:gene_aubes_nasa_image_rotor35.png?300 |}}
-<caption>Fig1. https://catalog.archives.gov/id/17466807 </caption>
+<caption>Fig. 1 https://catalog.archives.gov/id/17466807 </caption>
    * <code>@Misc{brown1977records,
 author   = {Brown, M.},