Wings

 

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Post-comp fixed wing

Wing design

@Nathaniel Li

Task Description

Design the wings of the post-comp fixed wing plane.

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Design integrates an 0.75”x0.75” aluminum box tube

@Nathaniel Li

Sep 8, 2024

Airfoil is based on a selected NACA airfoil

@Smile Khatri

Aug 26, 2024

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Task Progression/Updates

Author: @Nathaniel Li Updating Date: Aug 5, 2024

Updates from 2024-07-31 Mechanical Meeting Minutes and Designs

  • Plan to use 1/2” aluminum box tube for spars (also being used for frame)

  • @Sohee Yoon working on a design for balsa ribs

  • RPC laser cutters cuts up to 9.5mm thick pieces

    • If too thin, can glue two pieces together

  • Should keep in mind control surfaces that also need to be added (ie. ailerons and possibly flaps)

  • My current WIP design:

    • 0.23m chord length, 1.5m wingspan, NACA 4412 based on fixed wing calculator

      • Wingspan is end-to-end length but will most likely break into 2 sections so that it can connect to fuselage

    • 5mm rib thickness although 2-3mm (1/8”) seems common for rc planes with wingspan around 1-2m

      • Will look into what kind of Balsa sheets we can get, anything within 2-5mm range will do but should be able to get away with thinner side

      • Also can save lot of weight by cutting out material

    • Rib spacing is kinda unknown but ~ 2-3” and up to 5” is common

      • 5-10cm seems like a good range

    • Main issues to tackle:

      • Supporting LE and TE to prevent concaving issues

        • Thinking of doing a 3d print that covers them to give rigidity

      • Positioning of main and rear spar as discussed with @Smile Khatri → seems like 25-30% of chord length is ideal for main spar

        • For simplicity, usually a spar at LE and TE would suffice and also give the desired profile (and rigidity) but cutting the profile is very hard for Balsa tubes

 

 

 

 

 

 

 

 

Author: @Sohee Yoon Updating Date: Aug 6, 2024

Balsa Ribs Update

  • Designed a cut-out for the ribs. Based on this research article, elliptical cut-out shapes result in lower stresses in the aircraft ribs (studied using ANSYS) since sharp corners was what leads to higher stresses. Hence, I used elliptical cut-out shapes for our ribs. I also used a similar design in their studies (e.g., 3 ellipses) and chose the size in respect to their ratio between ellipses.

    • But…I did read on reddit that this doesn’t matter if your wingspan is greater than 6 inches…but that’s also from a random redditor

  • The placement of the ellipses solely depended on the spar cut-out and the thickness of the outline. There is at least 2-3 mm distance of clearance and 12.5 mm distance from the outer edge of an ellipse to another ellipse.

  • The ellipses and spar cut-our follow (or on) the camber line.

  • I wasn’t sure if the main spar and rear spar will be the same so I just made a cut-out with the one @Evan Janakievski added in the Wings file. This is welcome to change

    • I’m curious if we should fillet the corners to reduce stress but idk if the spar will fit

  • Thickness is 5 mm but we can def slim it down to 2-3 mm like @Nathaniel Li suggested

 

 

 

 

 

 

 

 

image-20240807-025757.png
Ribs

Wings Update

  • 8 ribs are spaced 80 mm apart and the wing skin is 600 mm (all are estimates rn)

 

 

 

 

 

 

 

 

image-20240807-030700.png
Wings

LE and TE Concave Issue

  • 3D prints that cover them is one solution but I was also considering a long wooden rod like in the images below and we can cut-out a circle in the front to insert it. But this will only for the the LE issues.

 

 

 

 

 

 

 

 

Control Surface Idea

 

 

 

 

 

 

 

 

Author: @Nathaniel Li Updating Date: Aug 10, 2024

Balsa Selection

 

 

 

 

 

 

 

 

LE and TE Concave Solution

  • Working on making a 3d print that would cover both LE and TE to preserve profile

 

 

 

 

 

 

 

 

Author: @Nathaniel Li Updating Date: Aug 19, 2024

3D Print Cover for LE and TE

  • 200mm length (print bed is 210mm x 210mm x 250mm for prusa)

  • LE follows curve profile and is 1mm thick into the rib

    • Not sure if 1mm is too thin/will fail easily but can always change to be thicker

  • TE is a triangular piece as following the curve profile would be too thin

  • Modelled in assembly

 

 

 

 

 

 

 

 

Weight Savings - 1/16” vs 1/8” ribs

  • Currently have 1/16” modelled

  • 1/16” rib weight: 0.795g

    • 0.795g x 8 ribs/wing x 2 wings = 12.72g

  • 1/8” rib weight: 1.591g

    • 1.591g x 8 ribs/wing x 2 wings = 25.456g

  • Total weight savings of 12.736g if using 1/16” instead of 1/8”

    • Tbh, this isn’t much of a weight savings so to be safe it might be better to go with 1/8” for more rigidity

 

 

 

 

 

 

 

 

Monokote and Ultracote

  • Monokote Covering This appears to be the monokote that other teams were talking about at comp

  • UltraCote White Ultracote is another material that kept coming up in my searches, it’s essentially the same product as monokote, it is the american name for Oracover (previously mentioned in our research)

  • Any hobbyist store would sell it, I found that Ricky's Hobby Corner has a lot of selection and is in Canada, they sell a variety of UltraCote

  • https://www.rcgroups.com/forums/showthread.php?2881437-Monokote-vs-Ultrakote

  • I think it’s worth using Ultracote for development as it’s easier to get started and will be faster for making a bunch of wings

  • In the future, we can look at using Monokote for a final product to make it more durable and look nicer (more colour selection apparently)

 

 

 

 

 

 

 

 

Author: @Alison Thompson Date: Aug 26, 2024

WING SYNC

Alison’s thoughts so far:

  • These are looking great!

  • Disagree on 12g being a small weight savings! 16th ribs > 1/8th ribs imo → this is 24g overall for the drone!

  • Don’t design around prusa dims, we should have bambu labs printer back

  • Unless you have a reason not to, I would make the cutouts larger but keep more vertical supports (more material in the vertical direction will help reduce bend more than more material in the horizonal direction, think like beam bending)

 

 

 

 

 

 

 

 

  • How are we thinking of adding ailerons to these?

  • How are we spacing out the ribs?

    • maybe LW PLA spacers?

  • TE print could probably be bigger, LE slightly thicker

  • How are the LE and TE prints attached? → glue

  • End cap + print that bolts to spar to keep wood on aluminum (shoutout Sohee)

  • You may want to make a test rib to check tolerance of the square cut-out after laser-cutting, talk to the person who does the laser cutting to find out what tolerances you can expect → exact sizing almost never just works for mating parts

  • tbh you addressed most of my concerns in design updates (no more second spar)

 

 

 

 

 

 

 

 

 

Author: @Evan Janakievski Date: Sep 8, 2024

  • Following deflection calculations for 1/2” box tube aluminum for 25 N (half of current lift force needed for cruising) and 68 N (calculated for just under half of lift force on take off), decided to update size of box tube to 3/4”

  • Deflection was up to 2 cm

  • Repeating tests (changed 68 N to 80 N for greater safety margin) with 3/4” box tube, deflection decreased to 2 mm

  • Files for sims on PDM in Fixed Wing → Wings

Author: @Sohee Yoon Date: Sep 11, 2024

  • Updated the wing cut outs, including spar, and the assembly

    • The cutout clearance is sketched below