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   Aircraft Dynamics Nomenclature PDF
Formulas : 18
Size : 381 kb
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Contents of the Aircraft Dynamics Nomenclature PDF

List of 18 Aircraft Dynamics Nomenclature Formulas

Aerodynamic Axial Force
​Go
Aerodynamic Normal Force
​Go
Aerodynamic Side Force
​Go
Angle of attack
​Go
Mean Aerodynamic Chord for Propeller-Driven Airplane
​Go
Normal Force Coefficient with Aerodynamic Normal Force
​Go
Pitching moment
​Go
Pitching moment coefficient
​Go
Rolling Moment
​Go
Rolling moment coefficient
​Go
Side force coefficient
​Go
Sideslip angle
​Go
Velocity along Pitch Axis for Small Sideslip Angle
​Go
Velocity along Roll Axis for Small Angle of Attack
​Go
Velocity along Roll Axis for Small Sideslip Angle
​Go
Velocity along Yaw Axis for Small Angle of Attack
​Go
Yawing Moment
​Go
Yawing moment coefficient
​Go

Variables used in Aircraft Dynamics Nomenclature PDF

  1. b Wingspan (Meter)
  2. Cm Pitching Moment Coefficient
  3. cma Mean Aerodynamic Chord (Meter)
  4. Cn Yawing Moment Coefficient
  5. Cx Axial Force Coefficient
  6. Cy Side Force Coefficient
  7. Cz Normal Force Coefficient
  8. C𝒍 Rolling Moment Coefficient
  9. Lc Chord Length (Meter)
  10. q Dynamic Pressure (Pascal)
  11. S Reference Area (Square Meter)
  12. u Velocity Along Roll Axis (Meter per Second)
  13. v Velocity Along Pitch Axis (Meter per Second)
  14. w Velocity Along Yaw Axis (Meter per Second)
  15. X Aerodynamic Axial Force (Newton)
  16. Y Aerodynamic Side Force (Newton)
  17. Z Aerodynamic Normal Force (Newton)
  18. α Angle of Attack (Degree)
  19. β Sideslip Angle (Degree)
  20. 𝑳 Rolling Moment (Newton Meter)
  21. 𝑴 Pitching Moment (Newton Meter)
  22. 𝑵 Yawing Moment (Newton Meter)
  23. 𝓁 Characteristic Length (Meter)

Constants, Functions and Measurements used in Aircraft Dynamics Nomenclature PDF

  1. Function: asin, asin(Number)
    The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio.
  2. Function: atan, atan(Number)
    Inverse tan is used to calculate the angle by applying the tangent ratio of the angle, which is the opposite side divided by the adjacent side of the right triangle.
  3. Function: int, int(expr, arg, from, to)
    The definite integral can be used to calculate net signed area, which is the area above the x -axis minus the area below the x -axis.
  4. Function: sin, sin(Angle)
    Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.
  5. Function: sqrt, sqrt(Number)
    A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
  6. Function: tan, tan(Angle)
    The tangent of an angle is a trigonometric ratio of the length of the side opposite an angle to the length of the side adjacent to an angle in a right triangle.
  7. Measurement: Length in Meter (m)
    Length Unit Conversion
  8. Measurement: Area in Square Meter (m²)
    Area Unit Conversion
  9. Measurement: Pressure in Pascal (Pa)
    Pressure Unit Conversion
  10. Measurement: Speed in Meter per Second (m/s)
    Speed Unit Conversion
  11. Measurement: Force in Newton (N)
    Force Unit Conversion
  12. Measurement: Angle in Degree (°)
    Angle Unit Conversion
  13. Measurement: Moment of Force in Newton Meter (N*m)
    Moment of Force Unit Conversion
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Free Aircraft Dynamics Nomenclature PDF

Get Free Aircraft Dynamics Nomenclature PDF for Download today. Examples are included after each Formula with a link to a live Calculator! All the Formulas and Calculators support Unit Conversion as well. This PDF features 18 calculators from Aircraft Mechanics. Inside, you'll discover a list of formulas such as Aerodynamic Axial Force, Aerodynamic Side Force and 18 more formulas!. The Variables, Functions and Constants are summarized at the end. Explore and share Aircraft Dynamics Nomenclature PDFs!

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