Speedy "Red Mini Wing" RC Plane

thingiverse

Here is the bird family brood with a crossbreed of the "Red Duck" and the "Red Swan." The offspring is still small but has gained incredible speed and agility - making it an excellent flight model for real pilots. A remarkable feat was accomplished by Marcel, a member of the ACNE group, who successfully piloted the maiden flight of this little wonder. As he reported, "This small model already shows exceptional qualities but some refinement would enhance its performance further." His feedback has guided us towards perfecting this hybrid brood. Here are the specifications for this extraordinary bird: Specifications: Airfoil: Clark YS Wing span: 794 mm Chord length: 160 mm Center of pressure: 27 mm Overall weight of wings: 270 g Surface area: 12.7 dm² Empty fuselage weight: 75 g Fuselage overall weight: 270 g Weight per unit area: 42.5 g/dm² Stability of flight (Thies): m=3 STFs. Our hybrid is designed to be powered by a Turnigy 2632 Brushless Motor 1000kv with an efficiency level close to optimal. We're using an Aeronaut Carbon Classic propeller, paired with the correct receiver, servos, and battery. Note that in order to produce perfect parts we will need precise control over layer heights and widths while maintaining smooth transitions from bottom to top sides as you move outward radially so layers don't start mid-air due. Here is a full listing of Print Settings to assist us all with this new design: Print Setting Guidelines 1. Wings (airfoils): Hollow structure - single perimeter, two bottom layers for stability. Top surfaces must have adequate adhesion through a continuous top layer to provide strength. Extrusion width at its highest (thickest). Inner support ribs merge both top and bottom seamlessly when properly aligned in sequence as you progress. 2. Ailerons: Hollow with an internal ribbed structure made up of 3 bottom layers with spiraling patterns which maintain constant speed allowing minimal infill or air gaps - ideal for minimizing unnecessary drag when aerodynamics require more lift rather than weight reduction since surface tension takes hold across flat smooth lines here too. Fuselage and associated appendages share print settings such as two perimeters one for each outer layer no bottom/top at 0.4 width, with ten percent infill; 5 layers beneath this exterior for strength before transitioning inward further until meeting solid support structure once finished inside totally sealing against unwanted leakage or seepage issues outside walls remain fully enclosed always thus completely secure throughout assembly phases required. Rafts must be omitted; Supports aren't recommended since structural stability through the main wing spar will provide all the necessary strength as per our unique internal spool structure keeping overall shape rigid enough to endure turbulence. Print at these precise specifications in order to have perfect models with great control: layer height=0.3mm width=0.5mm. Layer hight should be increased if needed since some users reported difficulty printing top side surfaces merging correctly, but always test prior! If there are further issues do experiment with slightly smaller or larger extrusion widths. Print thickness could be 0.49-48 for the sake of finding ideal parameters to fit individual user's slicing preferences successfully. This also will keep gaps in between top bottom and center layer small minimizing possible flaws from this minor error in setup entirely!