Timeline for Why does the rotor thrust decrease at smaller tip clearance for shrouded rotor?
Current License: CC BY-SA 4.0
5 events
| when toggle format | what | by | license | comment | |
|---|---|---|---|---|---|
| Jan 26, 2019 at 15:00 | history | tweeted | twitter.com/StackAviation/status/1089176320809099266 | ||
| Jan 24, 2019 at 13:59 | answer | added | Meatball Princess | timeline score: 2 | |
| Jan 16, 2019 at 10:21 | comment | added | Dat | @mins actually, the blade diameter is kept consant and the shroud diameter changes (the author used CFD and easily changed shroud diameter ) | |
| Jan 16, 2019 at 9:29 | comment | added | mins | "final question: why do we have increased inflow": When I read the excerpt and see your diagram, I understand that if you have a longer blade (resulting from a reduced clearance with constant shroud diameter), the rotor disk diameter is increased, hence the air flow mass (assuming the angular speed is kept constant). Am I wrong in my reading? | |
| Jan 16, 2019 at 8:13 | history | asked | Dat | CC BY-SA 4.0 |