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Understanding Lift and Drag

Jika Anda ingin melakukan itu, maka Anda akan memiliki lebih banyak lagi untuk mendukung Anda dan Anda akan memiliki lebih banyak lagi untuk Anda.

Calculating Lift and Drag Forces

Ini adalah kalkulated yang diikuti dengan formula ini:

Pertama; FLT: 0 = 0 = 0 × V ² S × C = FLT: 2 After3; LT: 1 1f 1; L1; L = 0.5 × V ² × C = 3 MIA 3O; 3; 3 3D;

S01. FLT: 0 = 0 × V ² × C = FLT: 2 Sym3; FLT: 1: 1 1; FL3; D = 0.5 × V ² × C × 3 = 3 = 333D; 3; 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3 = 3

Dimana:

  • Air Density
  • V = velocity of airflow
  • S = wing surface area
  • C 1f 1f; 1f; FLT: 0 = 33. L 1f; FLT: 1 = coefisien of lift
  • C 1f 1f; 1f; FLT: 0 = 33; D 1f; FLT: 1 = coefisien of drag

Calculating the Liftt -to-Drag Rasio

The lift -to -drag ratio (L / D) is obtained by dividding the lift force by the drag force:

L / D = C 1f 1; FLT: 0 AF3; L 1r; FLT: 1 After3; C 1; FLT: 2: 38.3; D CONT1; FLT: FLT: FLT: FLT; FL1; FL1; FL1; FLT: 3; 33; 193;

Application to Aerofoil Profiles

Diseduh aerosol profiles have unique C; FLT: 0: 3; L3; L 1; FLT: 1; 1; A3; C And 1; FLT: 2 Aver3; D3; DRD 1f proficeociciac-subset-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal-awal, dapat terjadi.