Hi, I’ve been developing an RV7 add-on for MS flight simulator, FSX...before I get started for real.
I know some folks are familiar with the project; it’s been in development a very-very long time - years![Smile :) :)](data:image/gif;base64,R0lGODlhAQABAIAAAAAAAP///yH5BAEAAAAALAAAAAABAAEAAAIBRAA7)
It’s sort of hard to believe but there are more hours in it now than a real one.
The biggest remaining task is defining all the aerodynamic coefficients.
While, I’m enjoying impersonating an aerospace engineer, it’s going to take more time than I’ve got to become one.
So I’m wondering, are these numbers already available somewhere?
If not, are they easily determined through experimentation?
Or, is there software that I could use to determine reasonable approximations.
I’m really hopeful there is software that can sort of lead me through this.
Right now I’m looking at Xfoil…and I will try AVL soon.
I’ll post a sample of the aerodynamics section.
I have a good idea of what each coefficient and tables means, I just don’t know yet the best way to determine them.
Below is the aerodynamics section; there is also a section for: ground effect, control surfaces, AOA, Mach, engine, and propeller.
Here’s a link to the complete set…http://msdn.microsoft.com/en-us/library/cc707067.aspx
Does this stuff look familiar to anyone?![Smile :) :)](data:image/gif;base64,R0lGODlhAQABAIAAAAAAAP///yH5BAEAAAAALAAAAAABAAEAAAIBRAA7)
Danny
For more project details...
http://www.baytower.ca/
forum
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2FAVL_MIT_RV7_2.jpg&hash=a58b2419e7f45446d7ff2707e95f47d3)
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2Frv7_10-6_exterior3.jpg&hash=fd5b415eb0164cbfd37363acad76550e)
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2Frv7_10-6_cockpit5.jpg&hash=3ed79f6020e49eff216915d848cb4c84)
I know some folks are familiar with the project; it’s been in development a very-very long time - years
It’s sort of hard to believe but there are more hours in it now than a real one.
The biggest remaining task is defining all the aerodynamic coefficients.
While, I’m enjoying impersonating an aerospace engineer, it’s going to take more time than I’ve got to become one.
So I’m wondering, are these numbers already available somewhere?
If not, are they easily determined through experimentation?
Or, is there software that I could use to determine reasonable approximations.
I’m really hopeful there is software that can sort of lead me through this.
Right now I’m looking at Xfoil…and I will try AVL soon.
I’ll post a sample of the aerodynamics section.
I have a good idea of what each coefficient and tables means, I just don’t know yet the best way to determine them.
Below is the aerodynamics section; there is also a section for: ground effect, control surfaces, AOA, Mach, engine, and propeller.
Here’s a link to the complete set…http://msdn.microsoft.com/en-us/library/cc707067.aspx
Does this stuff look familiar to anyone?
Danny
For more project details...
http://www.baytower.ca/
forum
Code:
;**** BEGINNING OF REQUIRED AERODYNAMICS ************************
;The following 6 blocks define the base stability and control derivatives
;Lift, Drag, Pitch, Side Force, Roll, and Yaw.
TOKEN_BEGIN AIR_80_LIFT_PARAMS
REAL8 0.000000 ; CL spoiler
REAL8 1.2 ; CL flaps
REAL8 0.000000 ; UNUSED
REAL8 0.715988 ; CLih
REAL8 -0.273018 ; CLde
REAL8 0.000000 ; UNUSED
TOKEN_END
TOKEN_BEGIN AIR_80_DRAG_PARAMS
REAL8 0.065 ; CDo
REAL8 0.07 ; CD flaps
REAL8 0.007000 ; CD gear
REAL8 0.000000 ; CD spoiler
TOKEN_END
TOKEN_BEGIN AIR_80_PITCH_PARAMS
REAL8 2.133893 ; CMih
REAL8 -1.6 ; CMde
REAL8 -0.051200 ; CMde due to propwash
REAL8 -2.601277 ; CLq
REAL8 0.988016 ; CL adot
REAL8 2.0 ; CM adot
REAL8 -28.770823 ; CMq
REAL8 -10.000000 ; CMq due to propwash
REAL8 0.0 ; CMo
REAL8 -0.07 ; CM flap
REAL8 -1.066947 ; CM delta trim
REAL8 0.020000 ; CM gear
REAL8 0.000000 ; CM spoiler
TOKEN_END
TOKEN_BEGIN AIR_80_SIDE_FORCE_PARAMS
REAL8 -0.569647 ; CyB
REAL8 0.038363 ; CyP
REAL8 0.018805 ; CyR
REAL8 -0.153025 ; Cy Delta Rudder
TOKEN_END
TOKEN_BEGIN AIR_80_ROLL_PARAMS
REAL8 0.045 ; ClB
REAL8 -0.9 ; ClP
REAL8 -0.061076 ; ClR
REAL8 0.000000 ; Cl Delta Spoiler
REAL8 -0.269225 ; Cl Delta Aileron
REAL8 0.010 ; Cl Delta Rudder
TOKEN_END
TOKEN_BEGIN AIR_80_YAW_PARAMS
REAL8 0.099757 ; CnB
REAL8 0.034553 ; CnP
REAL8 -0.524805 ; CnR
REAL8 -3.000000 ; CnR due to propwash
REAL8 0.000000 ; UNUSED
REAL8 0.000000 ; UNUSED
REAL8 -0.002345 ; Cn Delta Aileron
REAL8 0.063277 ; Cn Delta Rudder
REAL8 0.002048 ; Cn Delta Rudder due to propwash
TOKEN_END
;CL vs. Alpha
;The first entry defines the number of data points (maximum 47 entries)
TOKEN_BEGIN AIR_CL_ALPHA
dd 13 ; Number of Entries
REAL8 -3.142, 0.000
REAL8 -2.356, 0.500
REAL8 -1.571, 0.000
REAL8 -0.366, -1.528
REAL8 -0.078, 0.000
REAL8 0.017, 0.590
REAL8 0.262, 2.096
REAL8 0.288, 2.183
REAL8 0.314, 2.096
REAL8 0.340, 1.528
REAL8 1.571, 0.000
REAL8 2.356, -0.500
REAL8 3.142, 0.000
TOKEN_END
;CM vs. Alpha
;The first entry defines the number of data points (maximum 47 entries)
TOKEN_BEGIN AIR_CM_ALPHA
dd 13 ; Number of Entries
REAL8 -3.142, 0.000
REAL8 -0.550, -0.545
REAL8 -0.375, -0.545
REAL8 -0.305, -0.273
REAL8 -0.288, -0.227
REAL8 -0.271, -0.189
REAL8 0.000, 0.000
REAL8 0.271, 0.189
REAL8 0.288, 0.227
REAL8 0.305, 0.273
REAL8 0.375, 0.545
REAL8 0.550, 0.545
REAL8 3.142, 0.000
TOKEN_END
;**** END OF REQUIRED AERODYNAMICS ************************************************
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2FAVL_MIT_RV7_2.jpg&hash=a58b2419e7f45446d7ff2707e95f47d3)
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2Frv7_10-6_exterior3.jpg&hash=fd5b415eb0164cbfd37363acad76550e)
![](/community/proxy.php?image=http%3A%2F%2Fwww.baytower.ca%2Fphoto%2Frv7_10-6_cockpit5.jpg&hash=3ed79f6020e49eff216915d848cb4c84)
Last edited: