Différences

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

--- public:modeles:rotor_52:accueil [2024/07/30 11:41] – [Aerodynamic design] rafaelbarraud
+++ public:modeles:rotor_52:accueil [2024/07/30 11:43] (Version actuelle) – [Natural frequencies] rafaelbarraud
@@ Ligne 100: / Ligne 100: @@
 | 3     | 1T    | 7124.94                      | 1133.97                  |
+====Campbell diagram====
+Evolution of the natural frequencies of the first 3 vibration modes, as a function of rotation speed, for the mesh computed with OpenMCAD[(cite:Kojtych_2022_gene_aubes)]:
+{{ :public:modeles:rotor_52:campbell_eng_52_ref.png?500 }}
+<caption>Campbell diagram computed with a linear centrifugal preload, with clamped root (nominal rotation speed ωₙ = 1 020.1 rad/s)</caption>
+  * {{ :public:modeles:rotor_52:campbell_eng_52_ref.pdf |graph (.pdf)}}
+  * {{ :public:modeles:rotor_52:campbell_52_ref.csv |Campbell data (.csv)}}
@@ Ligne 128: / Ligne 136: @@
 | 3     | 1T    | 7148.25                      | 1137.68                  |
+====Campbell diagram====
+Comparison of the evolution of the natural frequencies of the first 3 vibration modes, as a function of rotation speed for the initial and the reference blade:
+{{ :public:modeles:rotor_52:campbell_eng_52_ini.png?500 }}
+<caption>Campbell diagram computed with a linear centrifugal preload, with clamped root (nominal speed ωₙ = 1 020.1 rad/s),
+initial blade (orange), reference blade (gray) </caption>
+  * {{ :public:modeles:rotor_52:campbell_eng_52_ini.pdf |graph (.pdf)}}
+  * {{ :public:modeles:rotor_52:campbell_52_ini.csv |Campbell data (.csv)}}