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Thrust and Power Requirements

Formulas : 19 Size : 347 kb

Coefficient of Drag due to Lift for Minimum Power required

Coefficient of Drag for given Thrust and Weight

Coefficient of Drag for given Thrust-to-Weight Ratio

Coefficient of Lift for given thrust and weight

Coefficient of Lift for given Thrust-to-Weight Ratio

Drag for Level and Unaccelerated Flight

Drag for Level and Unaccelerated Flight at Negligible Thrust Angle

Freestream Velocity given required Power

Freestream Velocity given Total Drag Force

Lift Coefficient given Minimum required Thrust

Lift for Level and Unaccelerated Flight at Negligible Thrust Angle

Lift for Unaccelerated Flight

Lift-Induced Drag Coefficient given required Thrust

Lift-to-Drag Ratio given required Thrust of Aircraft

Total Drag Force given required Power

Zero-lift drag coefficient at minimum required thrust

Zero-Lift Drag Coefficient for given Lift Coefficient

Zero-Lift Drag Coefficient for Minimum Power required

Zero-Lift Drag Coefficient given required Thrust

Constant: pi, 3.14159265358979323846264338327950288
Archimedes' constant
Function: cos, cos(Angle)
Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.
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.
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.
Measurement: Area in Square Meter (m²)
Area Unit Conversion
Measurement: Pressure in Pascal (Pa)
Pressure Unit Conversion
Measurement: Speed in Meter per Second (m/s)
Speed Unit Conversion
Measurement: Power in Watt (W)
Power Unit Conversion
Measurement: Force in Newton (N)
Force Unit Conversion
Measurement: Angle in Radian (rad)
Angle Unit Conversion