Rigidity and flexibility of CF Tubes


Author
Message
oekmont
oekmont
Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)
Group: Forum Members
Posts: 550, Visits: 27K
0°, as you are bending the tube.

Job_CF
J
Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)
Group: Forum Members
Posts: 6, Visits: 26
oekmont - 1/8/2018 2:16:19 PM
f=(F*l^3)/(3*E*I)
f= deflection
l= length between support and wheel
E= Young's modulus
I= Moment of inertia

E depends on the laminate
I know these two
MI for Solid Round Beams = (pi * (OD4 - ID4)) / 64
Deflection = (length^3 * force) / (3 * E * MI)
where
MI = Moment of Inertia
E = Modulas of Elasticity in psi

But two different Youngs Modulus figures given for this tube!
Youngs Modulus 0°(GPa)     90
Youngs Modulus 90°(GPa)   19
Which one to use?


oekmont
oekmont
Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)
Group: Forum Members
Posts: 550, Visits: 27K
f=(F*l^3)/(3*E*I)
f= deflection
l= length between support and wheel
E= Young's modulus
I= Moment of inertia

E depends on the laminate

Job_CF
J
Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)
Group: Forum Members
Posts: 6, Visits: 26
Yes, good idea to use Excel.
Due to the orientation of the fibers, 'Roll Wrapped' and 'Woven Finish' CF tubes have different ultimate tensile and compression strengths.
What are the appropriate formulae to use to calculate deflection load?
oekmont
oekmont
Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)
Group: Forum Members
Posts: 550, Visits: 27K
for iterations i simply use excel

Job_CF
J
Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)
Group: Forum Members
Posts: 6, Visits: 26
Does anyone know of a Round Tube Beams Deflection Calculator where material property values of a material (eg. roll wrapped of CF tube) can be entered manually?
Thanks!

oekmont
oekmont
Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)Supreme Being (3.4K reputation)
Group: Forum Members
Posts: 550, Visits: 27K
The landing is more of an energy problem, then an ultimate strength problem. The question is if the tube can store up enough energy before hitting the critical deflection (ground contact).

Edited 6 Years Ago by oekmont
Warren (Staff)
Warren (Staff)
Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)
Group: Administrators
Posts: 2.5K, Visits: 8K
The properties are similar based on our experience, due to similar construction (except for the surface finish).  However we do not have formal mechanical data for the woven finish tubes yet. 


Warren Penalver
Easy Composites / Carbon Mods - Technical Support Assistant
Job_CF
J
Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)Forum Member (38 reputation)
Group: Forum Members
Posts: 6, Visits: 26
Warren (Staff) - 1/4/2018 9:19:05 AM
I would be looking at our Roll Wrapped Carbon Fibre  range of tubes for this application.  Mechanical data is available for the tubes which means you can calculate the deflection based on the loads you are likely to experience. Remember that the static load weight you give will be considerably less than the experienced loading on initial landing impact so you will need to take this into account in your calculations.

Thanks Warren.
Heavy landing on one of the two rear wheels often happens in cross wind and turbulent conditions.
So for load, I will be using 6 x 170kg per wheel.
Are the mechanical properties for 25.0 mm OD  'Roll Wrapped' Carbon Fibre Tube same as for the 'Woven Finish' Roll wrapped Carbon Fibre Tube?
For calculating deflection, do I use Ult. Tensile and Compression Strength figures for 0°or 90°?
Thanks!

Edited 6 Years Ago by Job_CF
Warren (Staff)
Warren (Staff)
Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)Supreme Being (15K reputation)
Group: Administrators
Posts: 2.5K, Visits: 8K
I would be looking at our Roll Wrapped Carbon Fibre  range of tubes for this application.  Mechanical data is available for the tubes which means you can calculate the deflection based on the loads you are likely to experience. Remember that the static load weight you give will be considerably less than the experienced loading on initial landing impact so you will need to take this into account in your calculations.


Warren Penalver
Easy Composites / Carbon Mods - Technical Support Assistant
GO

Merge Selected

Merge into selected topic...



Merge into merge target...



Merge into a specific topic ID...




Similar Topics

Reading This Topic

Explore
Messages
Mentions
Search