General Adhesive Testing
Details
LOCTITE EA E-120HP - pasted and compressed between the panel and chassis
Epoxy-based
Typical “Apply, Fix, and Cure” adhesive
Material Characteristics & Notes
LOCTITE EA E-120HP
Superior thermal shock resistance
Excellent mechanical and electrical properties
Specifically peel and impact forces
Suitable for low stress [I wonder if that will be a problem.]
Withstands exposure to a wide variety of solvents and chemicals
Bonds dissimilar materials including aluminum, steel, and other metals, as well as a variety of plastics and ceramics
No mention of metal to organic compounds however
From Technical Data Sheet (TDS):
Modulus of Elasticity (general epoxy resins) - ~4.5 GPa
Shear Modulus (general epoxy resins) - ~2.1 GPa
Average Tensile Strength - 41 GPa
Lap Shear Strength (Stainless Steel) - 23 GPa
Bonding Characteristics & Notes
Cavities may have been unfilled by the adhesive
Cavities created by part geometry or air bubbles created by uneven adhesive application
Clamped and cured for at least 24 hours
Known Forces or Stresses
General tensile and compressive stresses due to general usage
Specific overloaded substrates may cause excess strain and/or malformation
General weight of hanging parts (eg. bottom panel)
Potential Forces or Stresses
Any random stresses due to car functions (eg. the wheels being bumped into the bottom panel while turning)
Any random stresses due to the environment (eg. driving over a large rock the presses against the bottom panel)
Quality and/or Physical Concerns
Neither yet
The chassis hasn’t been adhered to anything yet, so no quality concerns
Test(s)
Adhesive Yield Strength
Determine how much the adhesive can withstand
Tensile and shear stress must be tested
Yield is different for application, so maybe just figure out when it crosses a certain elongation?
Then find amount of force required
General Weight
Determine safety factor and actual elongation
Needed: surface area, bottom panel mass
Point Pressures
Determine ratio strain between overloaded and general sections
Quality
Determine air bubbles?
Determine shrinkage?
Testing Methods
MODS/Pre-calculations
[MAX ELONGATION AND DISPLACEMENT ARE BASED ON WHEN THE ADHESIVE BOND WOULD BREAK]
Constant elastic and shear modulus, max elongation of 3 mm, assumed height is 2 mm, max horizontal displacement of 1 mm, constant SA (in mm^2)
σ=Eε, σ=F/A, and ε=∆h/h
τ=Gγ, τ=F/A, and γ=∆x/h
Find F for both.
Constant SA (in mm^2), gravity is rounded to 9.8 m/s^2, mass unknown, constant elastic modulus, assumed height is 2 mm, average tensile strength of epoxy given
F=mg, σ=F/A, σ=Eε, and ε=∆h/h
SF=σ_avg/σ
N/A
SW
N/A
FEA of weight
N/A
Physical
Test amount of force required for adhesive to yield directly
Not needed.
Physical examinations
Expectations
MODS/Pre-calculations
I expect it to be a very large force needed in both cases
I expect the change in height to be extremely minimal, and the safety factor to be incredibly high
I don’t expect many air bubbles, but I expect a lot of missing edges
SW
Physical
Results
MODS/Pre-Calculations
Approximate Yield Forces: 1.38 giganewtons and 0.284 giganewtons (tensile and shear respectively)
Approximate Gravity-Induced Elongation: 0.241 nanometers
Approximate Gravity-Based Safety Factor: 76 million
N/A
SW
Physical
Analysis
MODS/Pre-Calculations
The force required to dislodge the adhesive from the carbon fiber sandwich or the chassis bars is incredibly huge. This much was expected. Meaning that for this scenario to happen, something truly drastic would have to happen to the car.
When sitting in place, the light bottom panel causes very little strain to the adhesive. The elongation seen isn’t even a nanometer. And in this scenario, the safety factor is almost 76 million!
N/A
SW
Physical