Différences
Ci-dessous, les différences entre deux révisions de la page.
Les deux révisions précédentes Révision précédente Prochaine révision | Révision précédente Prochaine révisionLes deux révisions suivantes | ||
ressources:logiciels:gene_aubes_nasa:geneaubeslisteaubes:rotor_4:accueil [2022/09/13 13:41] – [Original model] antoinelemery | ressources:logiciels:gene_aubes_nasa:geneaubeslisteaubes:rotor_4:accueil [2022/09/15 12:15] – antoinelemery | ||
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Ligne 9: | Ligne 9: | ||
<btn type=" | <btn type=" | ||
<modal id=" | <modal id=" | ||
- | **[[https:// | + | **[[https:// |
</ | </ | ||
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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. | 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:reid1978design>Reid. «Design and overall performance | + | * Original technical report [(cite:janetzke1972design>Janetzke. «Performance |
- | author | + | author |
- | title = {Design and overall performance | + | title = {Performance |
institution = {NASA Lewis Research Center Cleveland, OH, United States}, | institution = {NASA Lewis Research Center Cleveland, OH, United States}, | ||
- | note = {NASA-TP-1337, url~: \url{https:// | + | note = {NASA-TM X-2449, url~: \url{https:// |
</ | </ | ||
* Picture : | * Picture : | ||
Ligne 63: | Ligne 63: | ||
First three natural frequencies (with clamped root) for the mesh: | First three natural frequencies (with clamped root) for the mesh: | ||
- | - <fc # | + | - <fc # |
- | - <fc # | + | - <fc # |
- | - <fc # | + | - <fc # |
===== CAD ===== | ===== CAD ===== | ||
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<btn type=" | <btn type=" | ||
<modal id=" | <modal id=" | ||
- | **[[https:// | + | **[[https:// |
</ | </ | ||
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Ensuite, une autre série d' | Ensuite, une autre série d' | ||
- | * Rapport technique original [(cite:reid1978design>Reid. «Design and overall performance | + | * Rapport technique original [(cite:janetzke1972design>Janetzke. «Performance |
- | author | + | author |
- | title = {Design and overall performance | + | title = {Performance |
institution = {NASA Lewis Research Center Cleveland, OH, United States}, | institution = {NASA Lewis Research Center Cleveland, OH, United States}, | ||
- | note = {NASA-TP-1337, url~: \url{https:// | + | note = {NASA-TM X-2449, url~: \url{https:// |
</ | </ | ||
* Photographie : | * Photographie : | ||
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Fréquences des trois premiers modes (noeuds de la base encastrés) pour le maillage : | Fréquences des trois premiers modes (noeuds de la base encastrés) pour le maillage : | ||
- | - <fc # | + | - <fc # |
- | - <fc # | + | - <fc # |
- | - <fc # | + | - <fc # |
===== CAO ===== | ===== CAO ===== |
- public/modeles/rotor_04/accueil.txt
- Dernière modification : 2023/04/17 20:36
- de solenekojtych