Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Rushi Shah
K J Somaiya College of Engineering (K J Somaiya), Mumbai
Rushi Shah has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Total Surface Area of a Cone
Total Surface Area=pi*Radius*(Radius+sqrt(Radius^2+Height^2)) GO
Body Surface Area
Body Surface Area=0.007184*(Weight)^0.425*(Height)^0.725 GO
Lateral Surface Area of a Cone
Lateral Surface Area=pi*Radius*sqrt(Radius^2+Height^2) GO
Surface Area of a Capsule
Surface Area=2*pi*Radius*(2*Radius+Side) GO
Volume of a Capsule
Volume=pi*(Radius)^2*((4/3)*Radius+Side) GO
Volume of a Circular Cone
Volume=(1/3)*pi*(Radius)^2*Height GO
Base Surface Area of a Cone
Base Surface Area=pi*Radius^2 GO
Volume of a Circular Cylinder
Volume=pi*(Radius)^2*Height GO
Area of a Circle when radius is given
Area of Circle=pi*Radius^2 GO
Volume of a Hemisphere
Volume=(2/3)*pi*(Radius)^3 GO
Volume of a Sphere
Volume=(4/3)*pi*(Radius)^3 GO

11 Other formulas that calculate the same Output

Lift in an accelerated flight
Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle)) GO
Lift acting on aircraft during ground roll
Lift force=Weight-(Rolling Resistance/Coefficient of Rolling Friction) GO
Lift force for a body moving in a fluid of certain density
Lift force=lift coefficient*Reference Area*Density*(Velocity^2)/2 GO
Lift for an unaccelerated flight
Lift force=Weight-(Thrust of an aircraft*sin(Thrust angle)) GO
Lift for a level, unaccelerated flight at negligible thrust angle
Lift force=Dynamic Pressure*Area*lift coefficient GO
Lift Force
Lift force=lift coefficient*Dynamic Pressure*Area GO
Total Lift of wing-tail combination
Lift force=Lift due to wing+Lift due to tail GO
Lift force with angle of attack
Lift force=Drag Force*cot(Angle of attack) GO
Lift for given glide angle
Lift force=Drag Force/tan(Glide angle) GO
Lift during level turn
Lift force=Weight/cos(Bank angle) GO
Lift for a given load factor
Lift force=Load factor*Weight GO

Forces acting Perpendicular to the body on the flight path Formula

Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius)
L=W*cos(θ)-m*((v^2)/r)
More formulas
Forces acting on body along the flight path GO
Blunt-nosed radial coordinate flat plate (first approximation): GO
Pressure ratio of Blunt-nosed cylinder (first approximation): GO
Radial coordinate of Blunt-nosed cylinder (first approximation): GO
Radius of curvature for the sphere-cone body shape GO
Radius of curvature for the cylinder-wedge GO
Radius for the sphere-cone body shape GO
Radius for the cylinder-wedge body shape GO

What are the forces acting perpendicular to the body in flight?

There are many forces acting on the body during the flight including the drag, thrust, weight of body etc.

How to Calculate Forces acting Perpendicular to the body on the flight path?

Forces acting Perpendicular to the body on the flight path calculator uses Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius) to calculate the Lift force, The Forces acting Perpendicular to the body on the flight path formula is defined as the lift force minus the weight of the body at an inclination equal to the product mass of the body in hypersonic flow and velocity gradient. Lift force and is denoted by L symbol.

How to calculate Forces acting Perpendicular to the body on the flight path using this online calculator? To use this online calculator for Forces acting Perpendicular to the body on the flight path, enter Weight (W), Angle of Inclination (θ), Mass (m), Velocity (v) and Radius (r) and hit the calculate button. Here is how the Forces acting Perpendicular to the body on the flight path calculation can be explained with given input values -> -708999.760192 = 60*cos(1.56679952280753)-35.45*((60^2)/0.18).

FAQ

What is Forces acting Perpendicular to the body on the flight path?
The Forces acting Perpendicular to the body on the flight path formula is defined as the lift force minus the weight of the body at an inclination equal to the product mass of the body in hypersonic flow and velocity gradient and is represented as L=W*cos(θ)-m*((v^2)/r) or Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius). Weight is a body's relative mass or the quantity of matter contained by it, Angle of Inclination is formed by the inclination of one line to another; measured in degrees or radians, Mass is the quantity of matter in a body regardless of its volume or of any forces acting on it, Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). and Radius is a radial line from the focus to any point of a curve.
How to calculate Forces acting Perpendicular to the body on the flight path?
The Forces acting Perpendicular to the body on the flight path formula is defined as the lift force minus the weight of the body at an inclination equal to the product mass of the body in hypersonic flow and velocity gradient is calculated using Lift force=Weight*cos(Angle of Inclination)-Mass*((Velocity^2)/Radius). To calculate Forces acting Perpendicular to the body on the flight path, you need Weight (W), Angle of Inclination (θ), Mass (m), Velocity (v) and Radius (r). With our tool, you need to enter the respective value for Weight, Angle of Inclination, Mass, Velocity and Radius 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 Lift force?
In this formula, Lift force uses Weight, Angle of Inclination, Mass, Velocity and Radius. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Lift force=lift coefficient*Dynamic Pressure*Area
  • Lift force=(Mass*[g]*cos(Flight path angle))+(Mass*(Velocity^2)/Radius of Curvature)-(Thrust force*sin(Thrust angle))
  • Lift force=Weight-(Thrust of an aircraft*sin(Thrust angle))
  • Lift force=Dynamic Pressure*Area*lift coefficient
  • Lift force=Drag Force*cot(Angle of attack)
  • Lift force=Drag Force/tan(Glide angle)
  • Lift force=Weight-(Rolling Resistance/Coefficient of Rolling Friction)
  • Lift force=Weight/cos(Bank angle)
  • Lift force=Load factor*Weight
  • Lift force=Lift due to wing+Lift due to tail
  • Lift force=lift coefficient*Reference Area*Density*(Velocity^2)/2
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