Major aircraft wing types, their categories or descriptions, and their key advantages
and disadvantages:
✈️ Major Aircraft Wing Types
| Wing
   Type | Category
   / Description | Advantages | Disadvantages | 
| Straight / Rectangular | Constant chord, straight edges | Easy to design and build, good low-speed
  handling, predictable stall | High drag at high speeds, less efficient for
  fast flight | 
| Tapered | Chord decreases from root to tip | Lower induced drag, better aerodynamic
  efficiency, stronger wing root | More difficult to manufacture, tip stall
  risk | 
| Elliptical | Smooth oval-shaped planform | Best lift distribution, lowest induced drag | Very hard and expensive to manufacture | 
| Swept Back | Wings swept backward from root | Delays shockwaves, better high-speed and
  transonic performance | Reduced low-speed performance, risk of tip
  stall | 
| Swept Forward | Wings swept forward | Improved low-speed handling, delayed tip
  stall | Structural instability, increased wing flex,
  complex to build | 
| Delta | Triangular shape | Strong, excellent at supersonic speeds,
  large internal volume | High drag at low speeds, poor low-speed
  handling | 
| Variable Sweep | Wings can sweep backward or extend straight
  (swing wings) | Optimal performance at various speeds,
  versatile | Mechanically complex, heavy, expensive to
  maintain | 
| Canard | Small forewing near aircraft nose | Enhances maneuverability, provides extra
  lift | Can cause stability and trim issues, less
  efficient in conventional layouts | 
| Tandem | Two main wings, one in front of the other | Good lift-to-drag ratio, stable
  configuration | Rare, complex flight control, limited
  maneuverability | 
| Oblique | One wing swept forward, the other backward | Reduces wave drag at supersonic speeds,
  maintains subsonic performance | Very complex aerodynamically and
  mechanically, control difficulties | 
| High Wing | Mounted high on fuselage | Good ground clearance, stable, better
  downward lift distribution | Obstructed downward view, structurally
  heavier (needs stronger support) | 
| Low Wing | Mounted low on fuselage | Better visibility above, easier maintenance,
  easier ground access | More prone to ground damage, less stable on
  ground | 
| Biplane | Two stacked wings | High lift at low speeds, short wingspan,
  structurally strong | High drag, less efficient, outdated for
  high-speed aircraft | 
 
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