|
[Sponsors] |
April 21, 2018, 14:51 |
Thrust Coefficient vs. Drag Coefficient
|
#1 |
Member
Matt Ridzon
Join Date: Jun 2014
Posts: 91
Rep Power: 12 |
Admittedly, I'm ignorant of what the Thrust Coefficient of an airfoil is. I've only ever studied lift and drag coefficients of an airfoil, but never thrust coefficients in an academic setting. However, after a little digging through textbooks and some web searches, the thrust coefficient equation appears identical to that of the lift and drag coefficients. So intuition tells me the thrust acts opposite of drag, therefore the thrust coefficient would be identical to the drag coefficient but opposite in sign. Is my understanding correct?
Just as background information, here's what I'm doing...I am modeling an airfoil in Fluent and will extract its drag, lift, and thrust coefficients from steady-state laminar flow with low Re. Thanks in advance, M Ridzon |
|
April 23, 2018, 00:55 |
|
#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,741
Rep Power: 66 |
During aerial manuevers (i.e. turns, banks, loop-the-loops), part of the airfoil reaction forces can be in the direction of acceleration so that the thrust coefficient is not always equal and opposite the drag because the drag in the direction of the velocity.
The coefficients are all positive. |
|
April 23, 2018, 09:25 |
|
#3 | |
Member
Matt Ridzon
Join Date: Jun 2014
Posts: 91
Rep Power: 12 |
Quote:
M Ridzon |
||
April 23, 2018, 14:53 |
|
#4 |
New Member
Join Date: Mar 2018
Posts: 11
Rep Power: 8 |
Never heard of thrust coefficient for an airfoil. I've always used thrust coefficient for jet nozzle thrust. There is the concept of leading-edge suction for airfoils.
|
|
April 23, 2018, 15:22 |
|
#5 | |
Member
Matt Ridzon
Join Date: Jun 2014
Posts: 91
Rep Power: 12 |
Quote:
M Ridzon |
||
April 23, 2018, 17:20 |
|
#6 | |
New Member
Join Date: Mar 2018
Posts: 11
Rep Power: 8 |
Quote:
Just had another thought: for flapping wings, .e.g. birds and insects or ornithopters, the concept of thrust coefficient may be appropriate. Also for rotors and propellers which use airfoil sections |
||
April 24, 2018, 08:43 |
|
#7 |
Member
Matt Ridzon
Join Date: Jun 2014
Posts: 91
Rep Power: 12 |
Yes, thank you. My college colleague affirmed this also, noting that experts in the area of flapping wing technology use the idea of "thrust coefficient" to help define their research findings. And that is precisely the area of my current work is in.
|
|
April 24, 2018, 12:01 |
|
#8 | |
New Member
Join Date: Mar 2018
Posts: 11
Rep Power: 8 |
Quote:
Please keep us posted on your work! |
||
Tags |
drag coefficient, lift coefficient, thrust |
Thread Tools | Search this Thread |
Display Modes | |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Drag Coefficient Convergence Problem | John | FLUENT | 18 | June 24, 2023 09:22 |
wrong SU2 calculation for lift and drag coefficient for NAC4421 | mechy | SU2 | 7 | January 9, 2017 05:18 |
problem with saving drag coefficient | colopolo | FLUENT | 5 | April 12, 2013 10:59 |
Calculation of Drag Coefficient, Help Please | teek22 | CFX | 1 | April 26, 2012 18:41 |
Automotive test case | vinz | OpenFOAM Running, Solving & CFD | 98 | October 27, 2008 08:43 |