Différences

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

--- public:modeles:rotor_04:accueil [2023/02/24 20:46] – ikrambeghdadi
+++ public:modeles:rotor_04:accueil [2023/03/01 11:02] – solenekojtych
@@ Ligne 19: / Ligne 19: @@
 Then, another series of tests has been conducted with blade tip solidities of 1.3 (rotor 14), 1.5 (rotor 8), and 1.7 (rotor 12). Tip solidity are being changed by varying the number of blades while maintaining the same velocity diagrams and flow path. These stages were designed such that the tip solidity of both the rotor and stator blades are the same.
-  * Original technical report [(cite:janetzke1972design>Janetzke. «Performance of 1380-foot-per-second-tip-speed axial-flow compressor rotor with blade tip solidity of 1.1 » 1972.  {{ https://ntrs.nasa.gov/citations/19720011348|pdf}})]:
+  * Original technical report [(cite:janetzke1972design>Janetzke. «Performance of 1380-foot-per-second-tip-speed axial-flow compressor rotor with blade tip solidity of 1.1 » 1972.  {{ https://ntrs.nasa.gov/citations/19720011348|pdf}})]: <code>@TechReport{janetzke1972design,
-<code>@TechReport{janetzke1972design,
   author           = {Janetzke, David C. and Ball, Calvin L. and Hager, Roy D.},
   date             = {1972},
@@ Ligne 51: / Ligne 49: @@
 The geometry of rotor 4 is described in the [[https://ntrs.nasa.gov/citations/19720011348|original NASA report]]  by the following tables. The length are in inches and the angles in degrees.
 {{ :public:modeles:rotor_4:gene_aubes_nasa_geom_rotor4.png?400 |}}
-{{ :public:modeles:rotor_4:gene_aubes_nasa_geom_rotor3.png?400 |}}
 ===== Aerodynamic design  =====
@@ Ligne 195: / Ligne 193: @@
 ===== Propriétés matériau  =====
-Le matériau du rotor 4 est un alliage à base de nickel : un acier maraging de grade 200
+Le matériau du rotor 4 est un alliage à base de nickel : un acier maraging de grade 200.
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