Instruction - How to search for the Adverse Yaw numbers
- Use Microsoft Text Editor or I recommend download Notepad++
- Go to your Microsoft Flight Simulator installation folder
- Open Community, Official or specific aircraft folder depending on where you want to search
- Type in searchbar: flight_model.cfg
- Select one or all the cfg files, right click ‘‘Edit with Notepad++‘’
- Select ‘‘Search’’ in the taskmenu
- Type in: aileron_up_drag_coef
- Select ‘‘Keep Searching’’ or ‘‘Search in open files’’, write down / copy number
- Type in: aileron_down_drag_coef
- Select ‘‘Keep Searching’’ or ‘‘Search in open files’’, write down / copy number
- Type in: fuselage_lateral_cx
- Select ‘‘Keep Searching’’ or ‘‘Search in open files’’, write down / copy number
- Type in: CFD_ReinjectVTailX
- Select ‘‘Keep Searching’’ or ‘‘Search in open files’’, ‘’= 1’’ means vtail CFD activated
- Default numbers are:
aileron_up_drag_coef: 0.5
aileron_down_drag_coef: 1
fuselage_lateral_cx: 0.4
CFD_ReinjectVTailX = 1
any decrease of aileron up drag
and / or increase of aileron down drag means more adverse yaw
Important: Some Developers are using own Costum Codes,
which means the default values don’t have any effect,
these Airplanes are listed with CC
If an Aircraft doesn’t have any aileron up or down drag in the cfg file
it’s using default values = no adjustments were made to adverse yaw
or usage of own custom code
Feel free to share your numbers if they are not listed or got updated
via PM or in the comments. Thank you!
Explanation Videos - What is Adverse Yaw?
Adverse Yaw in MSFS
Adverse Yaw is a crucial feature which is often missing or not realistic enough in MSFS, you can make a smooth turn without having to use the rudder pedals at all, which can be completely unrealistic.
But excessive adverse yaw is not always needed in order to be realistic, also some aircraft have design features to minimize adverse yaw (differential ailerons, frise-type ailerons, flaperons, coupled ailerons and rudder). It also depends on other factors like aircraft geometry the aspect ratio of the wings.
SDK
Aerodynamics
aileron_up_drag_coef
Defines the drag added by upwards aileron deflection.
This parameter has a significant impact on adverse yaw.
Reduce upward deflection drag to get more adverse yaw.
This parameter is multiplied by the aileron deflection angle and internal coefficients.
Default is 0.5. This can be scaled with the aileron_up_drag_scalar parameter
in the [FLIGHT_TUNING] section and is further modified by internal coefficients.
aileron_down_drag_coef
Defines the drag added by upwards aileron deflection.
This parameter has a significant impact on adverse yaw.
Increase downward deflection drag to get more adverse yaw.
This parameter is multiplied by the aileron deflection angle.
Default is 1. This can be scaled with the aileron_down_drag_scalar parameter
in the [FLIGHT_TUNING] section and is further modified by internal coefficients.
fuselage_lateral_cx
Defines the perpendicular drag coefficient of the fuselage, which occurs when the airflow is going perpendicular to the front axis (ie: sideways - left to right or right to left) but also going up and down.
This coefficient has an impact on drag when side slipping, as well as a general impact on yaw stability and pitch stability.
Default is 0.4 - which is about the perpendicular drag of a cylinder - and the value should usually fall between 0.2 and 0.8 for most aircraft.
Suggestion: Asobo maybe did a mistake here,
0.8 is actually the drag of a cylinder, values should fall between 0.7 - 1.3 to be more realistic
(0.2 - 0.4 is the drag of a sphere (much too low for most airplanes)
drag_coef_zero_lift
Defines the target drag of the airplane in clean configuration (ie: no propeller, no turbulence, no engine wash, no gears, no flaps, no spoilers, no deflections…), when there is zero lift. This is usually also called the Cdo or Cd zerolift. Zero lift may occur at an angle of attack of zero - reason for which is sometimes the drag at an AoA of 0 - but most of the time, zero lift occurs at an angle of attack that is negative and the Cdo does not correspond to the drag at AoA 0.
In the legacy FSX flight model, this defines the actual Cdo.
In the modern flight model, this defines the target Cdo that will be distributed over all the surfaces of the aircraft when building the airplane used in the aerodynamic surface simulation. Once the aircraft is built, it will then be normalized to match exactly the target Cdo.
rudder_lift_coef
Defines the lift coefficient slope of the rudder control surface.
This will have a direct impact on rudder authority, yaw stability, adverse yaw and induced roll.
The rudder lift coefficient slope is usually dependent on the rudder aspect ratio and should be between 1.0 and 𝝅.
Default is 5.0, and generally values will always fall between 1.0 and 5.0, with a theoretical maximum of 2𝝅
and a recommended value between 2.0 (for less authority and stability) and 5.0 (for more authority and stability).
This can be scaled with the rudder_effectiveness parameter in the [FLIGHT_TUNING] section.
Airplane Geometry
wing_dihedral
This is the angle between the wing leading edge and a horizontal line parallel to the ground,
as seen when looking at the front of an aircraft. Technically defined as the dihedral angle Lambda, in degrees.
The wing dihedral impacts secondary effects such as induced roll and adverse yaw.
vtail_span
The vertical tail span is the vertical distance from the vertical tail-fuselage intersection
to the tip of the vertical tail, in ft. A large vtail span will impact the roll moment of the propeller wash
but also resist the aircraft roll movement. It will also counter adverse yaw and counter induced roll during rudder inputs.
Wishlist: Adverse Yaw - more improvements necessary
Adverse Yaw | Aircraft list
Latest Update: 16.06.23
Abbr. | flight_model.cfg | Deafult | More Adverse Yaw when |
---|---|---|---|
UD | aileron_up_drag_coef | 0.5 | decreased |
DD | aileron_down_drag_coef | 1 | increased |
FX | fuselage_lateral_cx | 0.4 | increased |
VT | CFD_ReinjectVTailX | vtail CFD | activated |
TA | Total Adverse Yaw | Rounded summary of in- & decrease (default + 0.5) |
CC | Custom Code | Custom Adverse Yaw simulation, UD & DD = no effect |
3rd Party
Developer_______ | Aircraft________________ | UD - DD_____ | TA/CC__ | FX__ | VT |
---|---|---|---|---|---|
Airmax514 | XB-70 Valkyrie | 0.5 - 2.5 | + 2 | 1.2 | |
Big Radials | Grumman JRF-6 Goose | 0.5 - 0.5 | 0 | 0.4 | |
Big Radials | Norseman | 0.5 - 1.5 | + 1 | 1.0 | |
Flyboy Simulations | Rans S6S Coyote II | 0.48 - 1.2 | + 0.7 | 0.52 | |
FlyingIron | F6F-5 Hellcat | - | CC | 0.55 | |
FlyingIron | P-38L | - | CC | 0.50 | |
FlyingIron | Spitfire MkIX | - | CC | 0.53 | |
Flysimware | Cessna 414 AW | 0.5 - 1 | + 0.5 | 0.2 | |
Got Friends | Discus-2c | - | CC | 0.55 | |
JustFlight | PA-28R Arrow III | 0.5 - 2.8 | + 2.3 | 0.57 | |
JustFlight | PA-28R Turbo Arrow III | 0.5 - 2.8 | + 2.3 | 0.57 | |
JustFlight | PA-28R Turbo Arrow IV | 0.2 - 3.9 | + 3.7 | 0.57 | |
Just Flight | PA-28 161 Warrior II | 0.5 - 2.8 | + 2.3 | 0.4 | |
Madolo & B21 | AS 33 Me | - | CC | 0.4 | |
Madolo & B21 | LS 4 | - | CC | - | |
Nemeth Designs | Partenavia P68B Victor | 0.5 - 2.0 | + 1.5 | 2.5 ? | |
PMDG | DC-6 | 0.41 - 0.81 | + 0.4 | 0.36 | |
SimWorks Studios | Kodiak 100 | 0.2 - 1.89 | + 1.7 | 0.4 | |
SimWorks Studios | RV-10 | 0 - 1.5 | + 1.5 | 0.6 | |
SimWorks Studios | RV-14 | - | CC | 0.2 |
Improvement Mods
Developer_______ | Aircraft________________ | UD - DD_____ | TA/CC__ | FX__ | VT |
---|---|---|---|---|---|
Black Square | Analog Caravan | 0.5 - 2.0 | + 1.5 | 0.4 | |
Black Square | Analog KingAir | 0.5 - 2.0 | + 1.5 | 0.4 | |
GotGravel | Monster NXCub | - | CC | 0.55 | |
GotGravel | Savage Carbon | - | CC | 0.6 | |
MrTommymxr | DA40-NGX | 1.5 - 2.0 | + 0.5 | 0.4 | |
MrTommymxr | DA62X | 0.5 - 1.5 | + 1 | 0.5 | |
WB-Sim & JPL | Cessna 152 | 0.5 - 2.0 | + 1.5 | 0.4 | |
WB-Sim | Cessna 172 SP Classic | 0.5 - 2.5 | + 2 | 0.8 | |
WB-Sim | Cessna 172 SP Floats | 0.5 - 2.5 | + 2 | 1.0 |
MSFS Base & Premium
Developer_______ | Aircraft________________ | UD - DD_____ | TA/CC__ | FX__ | VT |
---|---|---|---|---|---|
Asobo | Cessna 152 | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | Cessna 152 Aerobat | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | Cessna 172 classic | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | Cessna 172 G1000 | 0.5 -1.5 | + 1 | 4.3 ? | |
Asobo | CJ4 | 0.7 - 1 | + 0.3 | - | |
Asobo | Curtiss JN-4 Jenny | 0.5 - 2.0 | + 1.5 | 3.0 ? | |
Asobo | Douglas DC3 | 0.011 - 0.005 | - 0.006 | 0.8 | |
Asobo | DG Aviation DG-1001E | 0.125 - 0.25 | + 0.1 | 0.45 | |
Asobo | DG Aviation LS8-18 | 0.125 - 0.25 | + 0.1 | 0.45 | |
Asobo | FA18 | 1.0 - 0.5 | - 0.5 | 0.4 | |
Asobo | Grand Caravan EX | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | Grumman G-21 Goose | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | KingAir 350 | 0.5 - 2.0 | + 1.5 | 0.4 | |
Asobo | TBM 930 | 0.5 - 2.0 | + 1.5 | 0.4 | |