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Society of Allied Weight Engineers, Inc.
Aerospace • Marine • Offshore • Land • Allied Industries
SAWE
Mass Properties and Automotive
Directional Stability
SAWE Paper 3765
2021 SAWE Tech Fair
Brian Paul Wiegand, PE
Northrop Grumman Corporation, Retired
SAWE
Background
Have written papers concerning automotive performance and the Mass Properties
significance to that performance:
• Acceleration (0-60 MPH, Quarter-Mile ET, Top Speed).
• Braking (60-0 MPH Distance).
• Lateral acceleration (Max Lat G’s, Roll Stiffness, Roll Gain).
• Road Shock and Vibration (Transmissibility/Gain, Gyroscopic Reaction, Road Contact).
• Ride (Pitch and Bounce, Frequency of Motions, “Flat Ride”).
• Crash Survival (Peak Deceleration, Head Injury Criterion, Neck Injury Criterion).
Now a paper on another aspect of automotive performance and the Mass
Properties significance to that performance:
• Automotive Directional Stability (Understeer Gradient)
2
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
SAWE
Automotive Directional Stability Theory
• Although the development of the automobile preceded that of the
aircraft, the development of automotive directional stability theory
lagged that of aircraft by about 35 years.
• Primary forces that determine the dynamic behavior of aircraft are
aerodynamically generated by pressure differentials acting over the
aerosurface areas. In contrast, the primary forces that determine the
dynamic behavior of automobiles are traction forces acting over the
tire-to-ground contact areas:
• First wind tunnel: National Physical Laboratory, UK, 1903.
• First tire test machine: researchers Becker, Fromm, and Maruhn, GR, 1931.
3
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
SAWE
Automotive Directional Stability Theory
• 1925 French researcher George Broulheit, develops “slip angle” concept.
• 1931 German researchers Becker, Fromm, and Maruhn develop first tire
testing machine.
• 1934 Maurice Olley of General Motors, develops “over/under/neutral
steer” behavior concepts, formulates “skidpad” testing for behavior.
• 1956 Leonard Segel of the Cornell Aeronautical Laboratory advances
modern automotive directional stability theory:
• “Theoretical Prediction and Experimental Substantiation of the Response of the
Automobile to Steering Control”, presented at the Institution of Mechanical
Engineers, London, UK.
4
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Key Historical Theory Development Points
SAWE
Significance:
Side Load results in
Lateral Traction Force
“Fy” causing Slip Angle
“ψ”
Automotive Directional Stability Theory
5
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
• Automotive Directional Stability begins with the Tire.
• Most fundamental Tire concept is “Slip Angle” (ψ):
SAWE
Automotive Directional Stability Theory
6

 “Lateral Traction Force vs. Slip Angle” behavior @ a
Constant Normal Load:
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Significance:
•Slip Angle = f (Lateral
Traction Force “Fy”)
•Cornering Stiffness =
“∂Fy/∂ψ”
SAWE
Automotive Directional Stability Theory
7
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
“Lateral Traction Force vs. Slip Angle” behavior @
Varying Normal Load:
Ref.: Campbell, Colin; The Sports Car,
Robert Bentley Inc., Cambridge,
Massachusetts, 1969, pg. 165.
Significance:
Happens to be tire of the
subject vehicle utilized by
this paper for simulated
stability testing.
SAWE
Automotive Directional Stability Theory
8
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
 Stability Behavior reveals itself under Side Load “Fd”:
Ref.: Taborek, Jaroslav J.;
Mechanics of Vehicles,
Penton Publishing Co.;
Cleveland, OH, 1957, pg. 23.
Significance:
Understeer,
Neutral Steer,
Oversteer.
SAWE
Automotive Directional Stability Theory
9
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
 That was Stability Theory as understood by Maurice
Olley et al circa 1934. It has certain deficiencies:
•Does not show the variation in stability
with speed.
•Does not include the effects of roll.
•Is only qualitative, not quantitative.
•Does not allow for variance front to rear in
suspension and/or tires.
SAWE
Automotive Directional Stability Theory
10
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
 Circa Leonard Segel’s 1956 paper a number of
quantitative measures, or metrics, of Automotive
Directional Stability were developed. The most
significant is the “Understeer Gradient” (Kus) in deg/g:
Ref.: SAE J670_JAN2008, para. 11.3.3.1, “Understeer/Oversteer Gradient”, symbol “U”.
SAWE
Automotive Directional Stability Theory
11
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
“Don’t let anyone persuade you that the skidpad
tests don’t mean anything. They mean pretty
much everything if we will just take the trouble to
interpret them.”
Maurice Olley
Ref.: Milliken and Milliken; Chassis Design Principles and Analysis, SAE R-206, pg 49. This quote was
found in a letter from Olley to a colleague that was written sometime in the early 1930’s.
SAWE
Automotive Directional Stability Theory
12
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Skidpad Testing:
Significance:
Centrifugal Force supplies
Side Load -
Fy = m a
a = V2/R
Side Load reveals Stability
behavior.
R
V
SAWE
Automotive Directional Stability Theory
13
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Construct Skidpad Simulation of a subject
vehicle undergoing Stability Testing.
Conduct Sensitivity Analysis for each of
18 parameters:
Total Weight, Sprung Weight, Unsprung Weight, Forward Unsprung
Weight, Rear Unsprung Weight, Total Weight LCG, Sprung Weight LCG,
Total Weight VCG, Sprung Weight VCG, Track, Front Track, Rear Track,
Roll Stiffness, Front Roll Stiffness, Rear Roll Stiffness, Roll Axis Height,
Front Roll Center Height, and Rear Roll Center Height.
SAWE
Automotive Directional Stability Theory
14
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Skidpad Simulation:
Significance:
Simulation is of Steady-State
condition, driven by “ay”
incrementation, terminates
when “ay = apotential” at front
or rear axle.
SAWE
Automotive Directional Stability Theory
15
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Subject Vehicle; Automobile Model:
1958 Jaguar XK150S
Nominal Parameter Values:
Wt =3639.80 lb
Wf = 1748.03 lb Wr = 1891.76 lb
Ws = 3117.93 lb
Wusf = 214.03 lb Wusr = 307.85 lb
LCG = 53.01 in VCG = 22.91 in
LCGs = 51.82 in VCGs = 24.62 in
husf = 12.62 in husr = 12.68 in
RG = 16.10 deg/g
Krollf = 276.59 lb-ft/deg
Krollr = 167.78 lb-ft/deg
Lwb = 102.00 in
tf = 51.75 in tr = 51.25 in
hrcf = -7.8 in hrcr = 14.4 in
hr = 20.66 in hra = 3.48 in
Nominal Mass Properties:
SAWE
Automotive Directional Stability Theory
16
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Subject Vehicle; Tire Model:
1958 Dunlop RS4 6.00×16 bias ply
Significance:
Data “pick-off”
of “Fy, ψ” points
at every 200 lb
in Normal Load
“N”.
SAWE
Automotive Directional Stability Theory
17
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Subject Vehicle; Tire Model:
1958 Dunlop RS4 6.00×16 bias ply
Significance:
Construction of a
Tire math Model
as appropriate for
Stability Analysis.
SAWE
FOR N = 0: ψ = 0
Cs = 0
FOR N = 200: ψ = 0.0000007298 Fy
3 - 0.0001649884 Fy
2 + 0.0373856159 Fy - 0.0569243091
Cs = (0.0000021894 Fy
2 - 0.0003299768 Fy + 0.0373856159)-1
FOR N = 400: ψ = 0.0000002013 Fy
3 - 0.0000831348 Fy
2 + 0.0238845288 Fy- 0.1077319068
Cs = (0.0000006039 Fy
2 - 0.0001662696 Fy + 0.0238845288)-1
FOR N = 600: ψ = 0.0000000900 Fy
3 - 0.0000470133 Fy
2 + 0.0176483212 Fy - 0.1059394999
Cs = (0.00000027 Fy
2 - 0.0000940266 Fy + 0.0176483212)-1
FOR N = 800: ψ = 0.0000000520 Fy
3 - 0.0000321034 Fy
2 + 0.0152816867 Fy - 0.1398755826
Cs = (0.000000156 Fy
2 - 0.0000642068 Fy + 0.0152816867)-1
FOR N = 1000: ψ = 0.0000000314 Fy
3 - 0.0000214695 Fy
2 + 0.0139331283 Fy - 0.1532355494
Cs = (0.0000000942 Fy2 - 0.000042939 Fy + 0.0139331283)-1
FOR N = 1200: ψ = 0.0000000181 Fy
3 - 0.0000128501 Fy
2 + 0.0130700607 Fy - 0.1445554791
Cs = (0.0000000543 Fy
2 - 0.0000257002 Fy + 0.0130700607)-1
FOR N = 1400: ψ = 0.0000000134 Fy
3 - 0.0000104467 Fy
2 + 0.0138562141 Fy - 0.1328149449
Cs = (0.0000000402 Fy2 - 0.0000208934 Fy + 0.0138562141)-1
FOR N = 1600: ψ =0.0000000233 Fy
3 - 0.0000198687 Fy
2 + 0.0175605669 Fy - 0.0919030834
Cs = (0.0000000699 Fy
2 - 0.0000397374 Fy + 0.0175605669)-1
FOR N = 1700: ψ = 0.0000000458 Fy
3 - 0.0000376466 Fy
2 + 0.0220521855 Fy - 0.0917899852
Cs = (0.0000001374 Fy
2 - 0.0000752932 Fy + 0.0220521855)-1
FOR N = 1900:
ψ = 0.000000326337885 Fy
3 - 0.000191622271760 Fy
2 + 0.044829711256039 Fy -
0.030653568375158
Cs = (0.000000979013655 Fy
2 - 0.00038324454352 Fy + 0.044829711256039)-1
Automotive Directional Stability Theory
18
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Subject Vehicle; Tire Model:
1958 Dunlop RS4 6.00×16 bias ply
Significance:
This is the resultant
Tire math Model as
appropriate for
Stability Analysis >>
SAWE
Automotive Directional Stability Theory
19
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Subject Vehicle; Tire Model, Traction Coef.:
Significance:
The Tire Lateral Traction
Coefficient Model is utilized
to find the tire traction force
potentials >>>>>>>>>>>>
μ = (b – m N)
Ref.: Lamar, Paul; “Aerodynamics & the Group Seven Racing Car”, The Aerodynamics of Sports & Competition Automobiles,
Proceedings of AIAA Symposium; Los Angeles, CA, 20 April 1968.
Pif = 40 psi Pir = 45 psi
bf = 1.0779 lb/lb br = 1.0570 lb/lb
mf = 0.000297 lb-1 mr = 0.000269 lb-1
Kzf = 1329 lb/in Kzr = 1471 lb/in
SAWE
Automotive Directional Stability Theory
20
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Sensitivity Analysis:
•“One-At-a-Time”(OAT) Method:
Modify input value, get new output value.
•“Input-Output Regression” Method:
Fit a linear line to input/output; R2 measure of linearity.
•Parameter Coupling/Uncoupling:
Some coupling must be maintained if results are to be correct
(Ex.: Sprung Wt, Sprung Wt VCG, Sprung Wt LCG, Unsprung Wt
VCG, etc. affect Roll Gain).
Some coupling must be broken if results are to be correct (Ex.:
Goland & Jindra coupled LCG to fwd/aft spring stiff balance).
SAWE
Automotive Directional Stability Theory
21
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Sensitivity Analysis Results:
•Top 4 Directional Stability parameters are
Mass Properties.
• Most influential parameter is Total Vehicle
Weight LCG; next most influential is
Sprung Weight LCG.
•Out of the 18 parameters, Mass Properties
rank 1,2,3,4,8,10,11,13, and 16 in Stability
Significance.
SAWE
Automotive Directional Stability Theory
22
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Sensitivity Analysis Results :
SAWE
Automotive Directional Stability Theory
23
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Q&A (5 min)
SAWE
Automotive Directional Stability Theory
24
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Back-up Slides
SAWE
Automotive Directional Stability Theory
25
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
The study of aircraft directional stability long preceded
the existence of any aircraft; Sir George Cayley (1773–
1857) published On Aerial Navigation in three parts
over 1809-1810. Frederick William Lanchester (1868-
1946) published Aerial Flight in two parts over 1906-
08, and George Hartley Bryan (1864–1928) published
Stability in Aviation in 1911. All of these studied the
principles of flight long before powered aircraft became
a reality. The Wright’s were well aware of the works of
Cayley, and possibly of Bryan, but initially they still flew
a highly unstable “Wright Flyer” (Kitty Hawk, 1903).
SAWE
Automotive Directional Stability Theory
26
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
• “Understeer Gradient” (Kus) is a quantitative stability metric expressed in
radians or degrees per “g”.
• “Characteristic Speed” (Vchar) is a metric, calculated at zero lateral
acceleration, for comparing understeering designs with respect to the exact
degree of understeer present.
• “Critical Speed” (Vcrit) is a speed, calculated at zero lateral acceleration, where
an oversteering vehicle can switch from initially controllable (slight oversteer) to
very unstable (high oversteer) behavior.
• “Steady-State Steering Angle” (δss) steering angle required to make steady-
state turn of radius “R” at “ay”; is an indicator of under/over steer and of steering
responsiveness.
• “Static Margin” (SM), is a quantitative stability metric like “Kus”, but is expressed
as a dimensionless fraction. It constitutes a direct borrowing from aircraft stability
theory, with traction forces substituted for aerodynamic forces.
Five Most Common Stability Metrics
SAWE
Automotive Directional Stability Theory
27
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
1958 Jaguar
XK150S
Suspension
Geometry
SAWE
Automotive Directional Stability Theory
28
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
1958 Jaguar
XK150S Mass
Properties as
Needed for
Skidpad
Simulation
SAWE
Automotive Directional Stability Theory
29
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Typical Variation
in Understeer
Gradient (Stability)
with Lateral
Acceleration (“ay”
in g’s):
Ref.: Wong, Jo Yung; Theory of Ground Vehicles, John Wiley & Sons Inc.; Hoboken, NJ, 2008, pg. 375.
SAWE
Automotive Directional Stability Theory
30
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
Road undulations result
in lateral force vectors
through the C.G.
Wind gusts result in
lateral force vectors
near the C.G.
SAWE
Automotive Directional Stability Theory
31
Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data

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MASS PROPERTIES and AUTOMOTIVE DIRECTIONAL STABILITY

  • 1. Society of Allied Weight Engineers, Inc. Aerospace • Marine • Offshore • Land • Allied Industries SAWE Mass Properties and Automotive Directional Stability SAWE Paper 3765 2021 SAWE Tech Fair Brian Paul Wiegand, PE Northrop Grumman Corporation, Retired
  • 2. SAWE Background Have written papers concerning automotive performance and the Mass Properties significance to that performance: • Acceleration (0-60 MPH, Quarter-Mile ET, Top Speed). • Braking (60-0 MPH Distance). • Lateral acceleration (Max Lat G’s, Roll Stiffness, Roll Gain). • Road Shock and Vibration (Transmissibility/Gain, Gyroscopic Reaction, Road Contact). • Ride (Pitch and Bounce, Frequency of Motions, “Flat Ride”). • Crash Survival (Peak Deceleration, Head Injury Criterion, Neck Injury Criterion). Now a paper on another aspect of automotive performance and the Mass Properties significance to that performance: • Automotive Directional Stability (Understeer Gradient) 2 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
  • 3. SAWE Automotive Directional Stability Theory • Although the development of the automobile preceded that of the aircraft, the development of automotive directional stability theory lagged that of aircraft by about 35 years. • Primary forces that determine the dynamic behavior of aircraft are aerodynamically generated by pressure differentials acting over the aerosurface areas. In contrast, the primary forces that determine the dynamic behavior of automobiles are traction forces acting over the tire-to-ground contact areas: • First wind tunnel: National Physical Laboratory, UK, 1903. • First tire test machine: researchers Becker, Fromm, and Maruhn, GR, 1931. 3 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data
  • 4. SAWE Automotive Directional Stability Theory • 1925 French researcher George Broulheit, develops “slip angle” concept. • 1931 German researchers Becker, Fromm, and Maruhn develop first tire testing machine. • 1934 Maurice Olley of General Motors, develops “over/under/neutral steer” behavior concepts, formulates “skidpad” testing for behavior. • 1956 Leonard Segel of the Cornell Aeronautical Laboratory advances modern automotive directional stability theory: • “Theoretical Prediction and Experimental Substantiation of the Response of the Automobile to Steering Control”, presented at the Institution of Mechanical Engineers, London, UK. 4 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Key Historical Theory Development Points
  • 5. SAWE Significance: Side Load results in Lateral Traction Force “Fy” causing Slip Angle “ψ” Automotive Directional Stability Theory 5 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data • Automotive Directional Stability begins with the Tire. • Most fundamental Tire concept is “Slip Angle” (ψ):
  • 6. SAWE Automotive Directional Stability Theory 6   “Lateral Traction Force vs. Slip Angle” behavior @ a Constant Normal Load: Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Significance: •Slip Angle = f (Lateral Traction Force “Fy”) •Cornering Stiffness = “∂Fy/∂ψ”
  • 7. SAWE Automotive Directional Stability Theory 7 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data “Lateral Traction Force vs. Slip Angle” behavior @ Varying Normal Load: Ref.: Campbell, Colin; The Sports Car, Robert Bentley Inc., Cambridge, Massachusetts, 1969, pg. 165. Significance: Happens to be tire of the subject vehicle utilized by this paper for simulated stability testing.
  • 8. SAWE Automotive Directional Stability Theory 8 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data  Stability Behavior reveals itself under Side Load “Fd”: Ref.: Taborek, Jaroslav J.; Mechanics of Vehicles, Penton Publishing Co.; Cleveland, OH, 1957, pg. 23. Significance: Understeer, Neutral Steer, Oversteer.
  • 9. SAWE Automotive Directional Stability Theory 9 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data  That was Stability Theory as understood by Maurice Olley et al circa 1934. It has certain deficiencies: •Does not show the variation in stability with speed. •Does not include the effects of roll. •Is only qualitative, not quantitative. •Does not allow for variance front to rear in suspension and/or tires.
  • 10. SAWE Automotive Directional Stability Theory 10 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data  Circa Leonard Segel’s 1956 paper a number of quantitative measures, or metrics, of Automotive Directional Stability were developed. The most significant is the “Understeer Gradient” (Kus) in deg/g: Ref.: SAE J670_JAN2008, para. 11.3.3.1, “Understeer/Oversteer Gradient”, symbol “U”.
  • 11. SAWE Automotive Directional Stability Theory 11 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data “Don’t let anyone persuade you that the skidpad tests don’t mean anything. They mean pretty much everything if we will just take the trouble to interpret them.” Maurice Olley Ref.: Milliken and Milliken; Chassis Design Principles and Analysis, SAE R-206, pg 49. This quote was found in a letter from Olley to a colleague that was written sometime in the early 1930’s.
  • 12. SAWE Automotive Directional Stability Theory 12 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Skidpad Testing: Significance: Centrifugal Force supplies Side Load - Fy = m a a = V2/R Side Load reveals Stability behavior. R V
  • 13. SAWE Automotive Directional Stability Theory 13 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Construct Skidpad Simulation of a subject vehicle undergoing Stability Testing. Conduct Sensitivity Analysis for each of 18 parameters: Total Weight, Sprung Weight, Unsprung Weight, Forward Unsprung Weight, Rear Unsprung Weight, Total Weight LCG, Sprung Weight LCG, Total Weight VCG, Sprung Weight VCG, Track, Front Track, Rear Track, Roll Stiffness, Front Roll Stiffness, Rear Roll Stiffness, Roll Axis Height, Front Roll Center Height, and Rear Roll Center Height.
  • 14. SAWE Automotive Directional Stability Theory 14 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Skidpad Simulation: Significance: Simulation is of Steady-State condition, driven by “ay” incrementation, terminates when “ay = apotential” at front or rear axle.
  • 15. SAWE Automotive Directional Stability Theory 15 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Subject Vehicle; Automobile Model: 1958 Jaguar XK150S Nominal Parameter Values: Wt =3639.80 lb Wf = 1748.03 lb Wr = 1891.76 lb Ws = 3117.93 lb Wusf = 214.03 lb Wusr = 307.85 lb LCG = 53.01 in VCG = 22.91 in LCGs = 51.82 in VCGs = 24.62 in husf = 12.62 in husr = 12.68 in RG = 16.10 deg/g Krollf = 276.59 lb-ft/deg Krollr = 167.78 lb-ft/deg Lwb = 102.00 in tf = 51.75 in tr = 51.25 in hrcf = -7.8 in hrcr = 14.4 in hr = 20.66 in hra = 3.48 in Nominal Mass Properties:
  • 16. SAWE Automotive Directional Stability Theory 16 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Subject Vehicle; Tire Model: 1958 Dunlop RS4 6.00×16 bias ply Significance: Data “pick-off” of “Fy, ψ” points at every 200 lb in Normal Load “N”.
  • 17. SAWE Automotive Directional Stability Theory 17 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Subject Vehicle; Tire Model: 1958 Dunlop RS4 6.00×16 bias ply Significance: Construction of a Tire math Model as appropriate for Stability Analysis.
  • 18. SAWE FOR N = 0: ψ = 0 Cs = 0 FOR N = 200: ψ = 0.0000007298 Fy 3 - 0.0001649884 Fy 2 + 0.0373856159 Fy - 0.0569243091 Cs = (0.0000021894 Fy 2 - 0.0003299768 Fy + 0.0373856159)-1 FOR N = 400: ψ = 0.0000002013 Fy 3 - 0.0000831348 Fy 2 + 0.0238845288 Fy- 0.1077319068 Cs = (0.0000006039 Fy 2 - 0.0001662696 Fy + 0.0238845288)-1 FOR N = 600: ψ = 0.0000000900 Fy 3 - 0.0000470133 Fy 2 + 0.0176483212 Fy - 0.1059394999 Cs = (0.00000027 Fy 2 - 0.0000940266 Fy + 0.0176483212)-1 FOR N = 800: ψ = 0.0000000520 Fy 3 - 0.0000321034 Fy 2 + 0.0152816867 Fy - 0.1398755826 Cs = (0.000000156 Fy 2 - 0.0000642068 Fy + 0.0152816867)-1 FOR N = 1000: ψ = 0.0000000314 Fy 3 - 0.0000214695 Fy 2 + 0.0139331283 Fy - 0.1532355494 Cs = (0.0000000942 Fy2 - 0.000042939 Fy + 0.0139331283)-1 FOR N = 1200: ψ = 0.0000000181 Fy 3 - 0.0000128501 Fy 2 + 0.0130700607 Fy - 0.1445554791 Cs = (0.0000000543 Fy 2 - 0.0000257002 Fy + 0.0130700607)-1 FOR N = 1400: ψ = 0.0000000134 Fy 3 - 0.0000104467 Fy 2 + 0.0138562141 Fy - 0.1328149449 Cs = (0.0000000402 Fy2 - 0.0000208934 Fy + 0.0138562141)-1 FOR N = 1600: ψ =0.0000000233 Fy 3 - 0.0000198687 Fy 2 + 0.0175605669 Fy - 0.0919030834 Cs = (0.0000000699 Fy 2 - 0.0000397374 Fy + 0.0175605669)-1 FOR N = 1700: ψ = 0.0000000458 Fy 3 - 0.0000376466 Fy 2 + 0.0220521855 Fy - 0.0917899852 Cs = (0.0000001374 Fy 2 - 0.0000752932 Fy + 0.0220521855)-1 FOR N = 1900: ψ = 0.000000326337885 Fy 3 - 0.000191622271760 Fy 2 + 0.044829711256039 Fy - 0.030653568375158 Cs = (0.000000979013655 Fy 2 - 0.00038324454352 Fy + 0.044829711256039)-1 Automotive Directional Stability Theory 18 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Subject Vehicle; Tire Model: 1958 Dunlop RS4 6.00×16 bias ply Significance: This is the resultant Tire math Model as appropriate for Stability Analysis >>
  • 19. SAWE Automotive Directional Stability Theory 19 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Subject Vehicle; Tire Model, Traction Coef.: Significance: The Tire Lateral Traction Coefficient Model is utilized to find the tire traction force potentials >>>>>>>>>>>> μ = (b – m N) Ref.: Lamar, Paul; “Aerodynamics & the Group Seven Racing Car”, The Aerodynamics of Sports & Competition Automobiles, Proceedings of AIAA Symposium; Los Angeles, CA, 20 April 1968. Pif = 40 psi Pir = 45 psi bf = 1.0779 lb/lb br = 1.0570 lb/lb mf = 0.000297 lb-1 mr = 0.000269 lb-1 Kzf = 1329 lb/in Kzr = 1471 lb/in
  • 20. SAWE Automotive Directional Stability Theory 20 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Sensitivity Analysis: •“One-At-a-Time”(OAT) Method: Modify input value, get new output value. •“Input-Output Regression” Method: Fit a linear line to input/output; R2 measure of linearity. •Parameter Coupling/Uncoupling: Some coupling must be maintained if results are to be correct (Ex.: Sprung Wt, Sprung Wt VCG, Sprung Wt LCG, Unsprung Wt VCG, etc. affect Roll Gain). Some coupling must be broken if results are to be correct (Ex.: Goland & Jindra coupled LCG to fwd/aft spring stiff balance).
  • 21. SAWE Automotive Directional Stability Theory 21 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Sensitivity Analysis Results: •Top 4 Directional Stability parameters are Mass Properties. • Most influential parameter is Total Vehicle Weight LCG; next most influential is Sprung Weight LCG. •Out of the 18 parameters, Mass Properties rank 1,2,3,4,8,10,11,13, and 16 in Stability Significance.
  • 22. SAWE Automotive Directional Stability Theory 22 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Sensitivity Analysis Results :
  • 23. SAWE Automotive Directional Stability Theory 23 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Q&A (5 min)
  • 24. SAWE Automotive Directional Stability Theory 24 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Back-up Slides
  • 25. SAWE Automotive Directional Stability Theory 25 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data The study of aircraft directional stability long preceded the existence of any aircraft; Sir George Cayley (1773– 1857) published On Aerial Navigation in three parts over 1809-1810. Frederick William Lanchester (1868- 1946) published Aerial Flight in two parts over 1906- 08, and George Hartley Bryan (1864–1928) published Stability in Aviation in 1911. All of these studied the principles of flight long before powered aircraft became a reality. The Wright’s were well aware of the works of Cayley, and possibly of Bryan, but initially they still flew a highly unstable “Wright Flyer” (Kitty Hawk, 1903).
  • 26. SAWE Automotive Directional Stability Theory 26 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data • “Understeer Gradient” (Kus) is a quantitative stability metric expressed in radians or degrees per “g”. • “Characteristic Speed” (Vchar) is a metric, calculated at zero lateral acceleration, for comparing understeering designs with respect to the exact degree of understeer present. • “Critical Speed” (Vcrit) is a speed, calculated at zero lateral acceleration, where an oversteering vehicle can switch from initially controllable (slight oversteer) to very unstable (high oversteer) behavior. • “Steady-State Steering Angle” (δss) steering angle required to make steady- state turn of radius “R” at “ay”; is an indicator of under/over steer and of steering responsiveness. • “Static Margin” (SM), is a quantitative stability metric like “Kus”, but is expressed as a dimensionless fraction. It constitutes a direct borrowing from aircraft stability theory, with traction forces substituted for aerodynamic forces. Five Most Common Stability Metrics
  • 27. SAWE Automotive Directional Stability Theory 27 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data 1958 Jaguar XK150S Suspension Geometry
  • 28. SAWE Automotive Directional Stability Theory 28 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data 1958 Jaguar XK150S Mass Properties as Needed for Skidpad Simulation
  • 29. SAWE Automotive Directional Stability Theory 29 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Typical Variation in Understeer Gradient (Stability) with Lateral Acceleration (“ay” in g’s): Ref.: Wong, Jo Yung; Theory of Ground Vehicles, John Wiley & Sons Inc.; Hoboken, NJ, 2008, pg. 375.
  • 30. SAWE Automotive Directional Stability Theory 30 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data Road undulations result in lateral force vectors through the C.G. Wind gusts result in lateral force vectors near the C.G.
  • 31. SAWE Automotive Directional Stability Theory 31 Society of Allied Weight Engineers, Inc. proprietary - Document contains no export controlled technical data

Editor's Notes

  1. Can peruse past papers to enlarge on automotive performance aspects affected by mass properties….
  2. Note that this is much like a stress-strain diagram…. Is valid just for one normal load value, so by itself is not of much use….
  3. Tire info now plotted differently showing variation in normal load effect…. Serendippidy
  4. Segel’s paper made much use of Static Margin…. The developer of Understeer Gradient is…..
  5. The centrifugal side load is resisted by the centripetal lateral traction forces at the tires, and causes vehicle roll and variation in tire normal loads, resulting in varying slip angle and cornering stiffness values. The
  6. Not exactly the significance; significance is that simulation provides a simulated side load….
  7. Mass Properties Model determination, test configuration Nominal Parameter Values
  8. How tire model is created…
  9. How tire model is created…
  10. Math model plus other tire parameters
  11. Traction Coef “mu” model…
  12. Some details on method, and on uncoupling hazard, is needed