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Les deux révisions précédentes Révision précédente Prochaine révision | Révision précédente | ||
public:modeles:rotor_11:accueil [2023/03/28 09:54] – solenekojtych | public:modeles:rotor_11:accueil [2023/04/15 13:52] (Version actuelle) – [Material properties] ikrambeghdadi | ||
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annulus area on the performance of axial-flow fan stages. A series of three stage: rotor 11, 16 and 17 were designed with a weight flow per unit annulus area of 198, 178, and 208 kilograms per second per square meter. All three stages were designed to produce a pressure ratio of 1.57, and all had the same meridional flow path geometry. | annulus area on the performance of axial-flow fan stages. A series of three stage: rotor 11, 16 and 17 were designed with a weight flow per unit annulus area of 198, 178, and 208 kilograms per second per square meter. All three stages were designed to produce a pressure ratio of 1.57, and all had the same meridional flow path geometry. | ||
- | * Original technical report [(cite: | + | * Original technical report [(cite: |
author | author | ||
date = {1973}, | date = {1973}, | ||
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title = {Performance of transonic fan stage with weight flow per unit annulus area of 198 kilograms per sercond per square meter (40.6 (lb/ | title = {Performance of transonic fan stage with weight flow per unit annulus area of 198 kilograms per sercond per square meter (40.6 (lb/ | ||
number | number | ||
- | url = {https:// | + | url = {https:// |
- | + | } | |
</ | </ | ||
* Picture : | * Picture : | ||
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==== Material properties | ==== Material properties | ||
- | The original material of the rotor 11 is not defined in the NASA report. | + | The original material of the rotor 11 is not defined in the NASA report. |
- | + | ||
- | Considered properties: | + | |
^ | ^ | ||
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===== À propos ===== | ===== À propos ===== | ||
- | + | Le rotor 16 fait partie d'un programme de recherche visant à étudier l' | |
- | Le rotor 11 fait partie d'un programme de recherche visant à étudier l' | + | |
* Rapport technique original [(cite: | * Rapport technique original [(cite: |
- public/modeles/rotor_11/accueil.txt
- Dernière modification : 2023/04/15 13:52
- de ikrambeghdadi