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   Thrust and Power Requirements PDF
Formulas : 19
Size : 0 kb
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Related PDFs (1)

Lift and Drag Requirements
Formulas : 19   Size : 346 kb

Contents of the Thrust and Power Requirements PDF

List of 19 Thrust and Power Requirements Formulas

Minimum Thrust of aircraft required
​Go
Minimum Thrust required for given Lift Coefficient
​Go
Minimum Thrust required for given weight
​Go
Power required for given aerodynamic coefficients
​Go
Power required for given required thrust of aircraft
​Go
Power required for given total drag force
​Go
Thrust Angle for Unaccelerated Level Flight for given Drag
​Go
Thrust Angle for Unaccelerated Level Flight for given Lift
​Go
Thrust for given coefficients of lift and drag
​Go
Thrust for Level and Unaccelerated Flight
​Go
Thrust of aircraft required for given Lift-to-drag ratio
​Go
Thrust of Aircraft required for given required Power
​Go
Thrust of Aircraft required for Level, Unaccelerated Flight
​Go
Thrust-to-weight ratio
​Go
Weight of Aircraft for given Coefficients of Lift and Drag
​Go
Weight of Aircraft for given Lift-to-Drag Ratio
​Go
Weight of aircraft for given required power
​Go
Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle
​Go
Weight of Aircraft in Level, Unaccelerated Flight
​Go

Variables used in Thrust and Power Requirements PDF

  1. A Area (Square Meter)
  2. AR Aspect Ratio of a Wing
  3. CD Drag Coefficient
  4. CD,0 Zero Lift Drag Coefficient
  5. CD,i Coefficient Of Drag Due to Lift
  6. CL Lift Coefficient
  7. e Oswald Efficiency Factor
  8. FD Drag Force (Newton)
  9. FL Lift Force (Newton)
  10. LD Lift-to-Drag Ratio
  11. P Power (Watt)
  12. Pdynamic Dynamic Pressure (Pascal)
  13. S Reference Area (Square Meter)
  14. T Thrust (Newton)
  15. TW Thrust-to-Weight Ratio
  16. V∞ Freestream Velocity (Meter per Second)
  17. Wbody Weight of Body (Newton)
  18. σT Thrust Angle (Radian)

Constants, Functions and Measurements used in Thrust and Power Requirements PDF

  1. Constant: pi, 3.14159265358979323846264338327950288
    Archimedes' constant
  2. Function: acos, acos(Number)
    The inverse cosine function, is the inverse function of the cosine function. It is the function that takes a ratio as an input and returns the angle whose cosine is equal to that ratio.
  3. 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.
  4. Function: cos, cos(Angle)
    Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.
  5. 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.
  6. Measurement: Area in Square Meter (m²)
    Area Unit Conversion
  7. Measurement: Pressure in Pascal (Pa)
    Pressure Unit Conversion
  8. Measurement: Speed in Meter per Second (m/s)
    Speed Unit Conversion
  9. Measurement: Power in Watt (W)
    Power Unit Conversion
  10. Measurement: Force in Newton (N)
    Force Unit Conversion
  11. Measurement: Angle in Radian (rad)
    Angle Unit Conversion
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Free Thrust and Power Requirements PDF

Get Free Thrust and Power Requirements 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 19 calculators from Aircraft Performance. Inside, you'll discover a list of formulas such as Thrust for Level and Unaccelerated Flight, Thrust Angle for Unaccelerated Level Flight for given Drag and 19 more formulas!. The Variables, Functions and Constants are summarized at the end. Explore and share Thrust and Power Requirements PDFs!

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