c130 airfoil 3d models

Here are the specific print settings for each part: * W1, W2: Four bottom layers and four top layers * W3 servo: Three bottom layers and four top layers * W4, W5: Three bottom layers and three top layers * W6: Three bottom layers and five top layers...

Specifications: * Airfoils: own design * Wing span: 1300 mm * Wing chord: 480/140 mm * CoG: 220 mm from the front of the fuselage * Overall weight: 1245 g * Wing weight one side complete: 342 g * Wing area: 32 dm² * Wing loading: 39 g/dm² * Motor:...

This idea was inspired by Flite Test sticking a KF airfoil on a plane, which made me think of swappable wings and this idea kicked off. The Body Lid has a servo slot so you can use one servo in the centre to control both ailerons. The Lid can be...

Things like making the vanes thinner, adding airfoil cross sections, sweeping the blades, playing with alpha and twist, all can be tailored to match a given fan. Instead what I tried brewing up here is something more generally applicable... ...a higher...

The long rectengular shape in the middle could get support because it is easy to take off. The Base part should get around 100°C (I used PLA) or even higher bed temperature to avoid the Warping effect. Turbine blade: Infill: 100% Layer hight 0.1mm...

2: 2,2260,416 (As rendered in Octane).\n\nAll glass geometry has thickness.\nThe Airfoil is rigged in Cinema 4D to extend and retract.\nAll wheels have proper pivot points and are ready for animation (Cinema 4D/FBX).\nFully unwrapped UV's are...

So you have to take it from here: https://www.thingiverse.com/thing:4280142 Specifications airfoils: own design wing span: 1600 mm wing chord: 284/140 mm CoG: 190 mm from rear edge of the fuselage overall weight: 870 g (PETG/LW PLA) wing area: 35...

More informations https://www.rc-network.de/threads/andreas-delta.11822532/ https://www.rcgroups.com/forums/showthread.php?3754295-Andreas-Delta Specifications airfoil: NACA 0006 wing span: 1100 mm wing chord: 680/200 mm CoG: 460 mm from rear...

The airfoils are the same, the washout, the angles - all the same as the original, only 1.3 meters instead of 2 meter span. I'm also including in this listing factory files so you can print tune the settings to your printer and G-code files for a...

Rotor: The rotor consists of three NACA 0015 airfoils, which are extruded into a helix with four parts each and an overall height of 80 cm. Each of the middle three parts of the helix blade requires the "helix blade" and "helix blade 2" parts to be...

The fuse profile is very close and the airfoil is the original Aquila shape with just a little thickness added. The size is based on a 400mm wing span. It's a two piece wing. 200mm is a big as I can print on my Ender 3. It does fly...

I did some additional research and found out that most professional vawts have a starting mechanism, because their efficiency comes only from airfoil profile which has to generate alot of torque from a standing start(printed bearings also don't help...

The little bulges on the fins are wrong though, and I don't have information on the airfoil used for the fins, so I used the Swept Naca shape in tinkercad as my bases for the fins, then cut out chunks to get the correct final shape (retaining the...

Based on the DC-10, it features a stretched fuselage, increased wingspan with winglets, refined airfoils on the wing and smaller tailplane, new engines and increased use of composite materials. Two of its engines are mounted on underwing pylons and a...

It is a ground-up aerodynamic design with its own tailored airfoil set, and wing planform. It features slightly more wingspan and wing area than the famed Nano Goblin to put up with the extra weight. On average, wing loading should be very similar,...

Specifications airfoils: own design wing span: 2000 mm wing chord: 284/140 mm CoG: 198 mm from rear edge of the fuselage motor camber: -4.6° (long fuselage front version 205 mm) overall weight: 1140 g (PETG/LW PLA) wing area: 45,5 dm² wing loading:...

Specifications airfoils: own design wing span: 2000 mm wing chord: 284/140 mm CoG: 198 mm from rear edge of the fuselage motor camber: -4.6° (long fuselage front version 205 mm) overall weight: 1140 g (PETG/LW PLA) wing area: 45,5 dm² wing loading:...

The best way to goRA30 - a slight twist, a gentle rotationRA70 - a steep rotation, will probably end up shredded by any launchFor all of the challenge outcomes, we used the V1-SO65-H100-RA00 model.Further refinementAfter the competition, I refined...

The part cooler is an airfoil that envelopes the nozzle in a 360 degree radius and is somewhat similar to the way a “bladeless” Dyson fan works. The design fits closely to the nozzle of the Revo which means you absolutely must print the part cooler...