-
-
June 16, 2020 at 5:56 am
baeblue321
SubscriberHi, well I have simulation a blade that the inlet's boundary condition is Pressure Inlet and the outlet is Mass Flow. But the problem is in my boundary condition I put the pressure in Gauge Total Pressure is 96483 Pa but when i saw in the result the pressure inlet is getting decrease (72830 Pa). anybody know why my pressure inlet didn't lock into 96483 ? I really need ur help. Thanks
-
June 17, 2020 at 12:53 am
Karthik Remella
AdministratorIs your flow incompressible or compressible? And, are you observing a dip in the static pressure value (72830 Pa)?
Thanks.
Karthik
Â
-
June 17, 2020 at 2:28 pm
baeblue321
Subscriberits a compressible and actually the fluid is a steam. I'm curios why the inlet fluid is changed while i set in the pressure inlet. Is it possible if the problem was because i used the material is air? because i still cant decide what fluid i used if the fluid is steam
-
June 19, 2020 at 12:10 pm
Karthik Remella
AdministratorIf your fluid is steam, please use the properties of steam. I'm assuming that the velocity of the fluid is high and therefore, the flow is compressible. Is that correct?
Thanks.
Karthik
-
June 20, 2020 at 3:32 pm
baeblue321
Subscribersorry, i was wrong the fluid actually a gas that contain a little SO2, the velocity for one blade i assume around 26,5 m/s and the yes the flow is compressible. I put the air as material fluid cause i assume both of gas and air same, correct me if i was wrong
-
June 21, 2020 at 5:25 am
-
June 21, 2020 at 10:28 pm
Karthik Remella
AdministratorCould you please perform the same using the variable 'Total Pressure' and not 'Pressure'? Are you getting a value which is closer?
Thanks.
Karthik
-
June 22, 2020 at 5:01 pm
baeblue321
SubscriberThe option for pressure only Pressure -
June 25, 2020 at 1:01 pm
Rob
Forum ModeratorClick on the button with the ... next to "Pressure".
-
- The topic ‘Pressure get decrease in result’ is closed to new replies.
-
5834
-
1906
-
1420
-
1305
-
1021
© 2026 Copyright ANSYS, Inc. All rights reserved.

