Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Sai Venkata Phanindra Chary Arendra
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Diagonal of a Rectangle when breadth and area are given
Diagonal=sqrt(((Area)^2/(Breadth)^2)+(Breadth)^2) GO
Diagonal of a Rectangle when length and area are given
Diagonal=sqrt(((Area)^2/(Length)^2)+(Length)^2) GO
Side of a Kite when other side and area are given
Side A=(Area*cosec(Angle Between Sides))/Side B GO
Perimeter of rectangle when area and rectangle length are given
Perimeter=(2*Area+2*(Length)^2)/Length GO
Buoyant Force
Buoyant Force=Pressure*Area GO
Perimeter of a square when area is given
Perimeter=4*sqrt(Area) GO
Diagonal of a Square when area is given
Diagonal=sqrt(2*Area) GO
Length of rectangle when area and breadth are given
Length=Area/Breadth GO
Breadth of rectangle when area and length are given
Breadth=Area/Length GO
Pressure when force and area are given
Pressure=Force/Area GO
Stress
Stress=Force/Area GO

11 Other formulas that calculate the same Output

Drag during ground effect
Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area) GO
Drag in an accelerated flight
Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) GO
Drag force on the plate in boundary layer flow
Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number) GO
Drag force in falling sphere resistance method
Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere GO
Forces acting on body along the flight path
Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient) GO
Drag for a level, unaccelerated flight
Drag Force=Thrust of an aircraft*(cos(Thrust angle)) GO
Drag force
Drag Force=Drag Coefficient*Dynamic Pressure*Area GO
Total Drag for given excess power
Drag Force=Thrust force-(Excess Power/Velocity) GO
Drag force with angle of attack
Drag Force=Lift force/cot(Angle of attack) GO
Drag for given glide angle
Drag Force=Lift force*tan(Glide angle) GO
Total drag for given required power
Drag Force=Power/Freestream Velocity GO

Drag for a level, unaccelerated flight at negligible thrust angle Formula

Drag Force=Dynamic Pressure*Area*Drag Coefficient
F<sub>D</sub>=P<sub>dynamic*A*C<sub>D</sub>
More formulas
Coefficient of Drag for given thrust-to-weight ratio GO
Coefficient of Drag for given thrust and weight GO
Zero-lift drag coefficient for given required thrust GO
Lift-induced drag coefficient for given required thrust GO
Zero-lift drag coefficient for given lift coefficient GO
Zero-lift drag coefficient at minimum required thrust GO

Does drag increase with altitude?

The Reynolds-Number decreases with an increasing altitude, which means that drag increases with an increasing altitude.

How to Calculate Drag for a level, unaccelerated flight at negligible thrust angle?

Drag for a level, unaccelerated flight at negligible thrust angle calculator uses Drag Force=Dynamic Pressure*Area*Drag Coefficient to calculate the Drag Force, The Drag for a level, unaccelerated flight at negligible thrust angle is the product of dynamic pressure, reference area, and drag coefficient. Drag Force and is denoted by FD symbol.

How to calculate Drag for a level, unaccelerated flight at negligible thrust angle using this online calculator? To use this online calculator for Drag for a level, unaccelerated flight at negligible thrust angle, enter Dynamic Pressure (Pdynamic), Area (A) and Drag Coefficient (CD) and hit the calculate button. Here is how the Drag for a level, unaccelerated flight at negligible thrust angle calculation can be explained with given input values -> 50000 = 10*50*100.

FAQ

What is Drag for a level, unaccelerated flight at negligible thrust angle?
The Drag for a level, unaccelerated flight at negligible thrust angle is the product of dynamic pressure, reference area, and drag coefficient and is represented as FDdynamic*A*CD or Drag Force=Dynamic Pressure*Area*Drag Coefficient. Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid, The area is the amount of two-dimensional space taken up by an object and Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
How to calculate Drag for a level, unaccelerated flight at negligible thrust angle?
The Drag for a level, unaccelerated flight at negligible thrust angle is the product of dynamic pressure, reference area, and drag coefficient is calculated using Drag Force=Dynamic Pressure*Area*Drag Coefficient. To calculate Drag for a level, unaccelerated flight at negligible thrust angle, you need Dynamic Pressure (Pdynamic), Area (A) and Drag Coefficient (CD). With our tool, you need to enter the respective value for Dynamic Pressure, Area and Drag Coefficient and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Drag Force?
In this formula, Drag Force uses Dynamic Pressure, Area and Drag Coefficient. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Drag Force=Drag Coefficient*Dynamic Pressure*Area
  • Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient)
  • Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration)
  • Drag Force=Thrust of an aircraft*(cos(Thrust angle))
  • Drag Force=Lift force/cot(Angle of attack)
  • Drag Force=Power/Freestream Velocity
  • Drag Force=Thrust force-(Excess Power/Velocity)
  • Drag Force=Lift force*tan(Glide angle)
  • Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area)
  • Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere
  • Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number)
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