Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Sai Venkata Phanindra Chary Arendra
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
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11 Other formulas that you can solve using the same Inputs

Pressure when density and height are given
Pressure=Density*Acceleration Due To Gravity*Height GO
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
Molar Volume
Molar Volume=(Atomic Weight*Molar Mass)/Density 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
Pressure when force and area are given
Pressure=Force/Area GO
Stress
Stress=Force/Area GO

2 Other formulas that calculate the same Output

Normal Force Coefficient
coefficient of force=Normal Force/(Dynamic Pressure*Area) GO
Axial force coefficient
coefficient of force=Force/(Dynamic Pressure*Area) GO

Doty and Rasmussen - normal-force coefficient Formula

coefficient of force=2*Normal Force/(Density*(Freestream Velocity^2)*Area)
CN=2*Fn/(ρ*(V<sub>∞</sub>^2)*A)
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Non dimensional Change in hypersonic disturbance velocity in x direction GO
Non dimensional Change in hypersonic disturbance velocity in y direction GO
Non dimensional pressure equation with slenderness ratio GO
Non dimensional Velocity disturbance in y direction in hypersonic flow GO
Coefficient of pressure with slenderness ratio GO
Coefficient of pressure with slenderness ratio and similarity constant GO
Similarity constant equation using the wave angle GO
Rasmussen closed-form expression for the shock-wave angle GO
Inverse of density for hypersonic flow GO
Inverse of density for hypersonic flow using mach number GO
Constant g used for finding the location of perturbed shock GO
Non- dimensionalised time GO
Distance from tip of the leading edge to the base GO

What is a normal force?

The normal force is the support force exerted upon an object that is in contact with another stable object. For example, if a book is resting upon a surface, then the surface is exerting an upward force upon the book in order to support the weight of the book.

How to Calculate Doty and Rasmussen - normal-force coefficient ?

Doty and Rasmussen - normal-force coefficient calculator uses coefficient of force=2*Normal Force/(Density*(Freestream Velocity^2)*Area) to calculate the coefficient of force, The Doty and Rasmussen - normal-force coefficient formula is defined as the ratio of double the normal force acting on the body to the product of density, the square of the velocity of freestream and reference area. coefficient of force and is denoted by CN symbol.

How to calculate Doty and Rasmussen - normal-force coefficient using this online calculator? To use this online calculator for Doty and Rasmussen - normal-force coefficient , enter Normal Force (Fn), Density (ρ), Freestream Velocity (V) and Area (A) and hit the calculate button. Here is how the Doty and Rasmussen - normal-force coefficient calculation can be explained with given input values -> 2.006E-7 = 2*50/(997*(100^2)*50).

FAQ

What is Doty and Rasmussen - normal-force coefficient ?
The Doty and Rasmussen - normal-force coefficient formula is defined as the ratio of double the normal force acting on the body to the product of density, the square of the velocity of freestream and reference area and is represented as CN=2*Fn/(ρ*(V^2)*A) or coefficient of force=2*Normal Force/(Density*(Freestream Velocity^2)*Area). Normal Force is the force which is normal to the shear force. , The density of a material shows the denseness of that material in a specific given area. This is taken as mass per unit volume of a given object. , The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air and The area is the amount of two-dimensional space taken up by an object.
How to calculate Doty and Rasmussen - normal-force coefficient ?
The Doty and Rasmussen - normal-force coefficient formula is defined as the ratio of double the normal force acting on the body to the product of density, the square of the velocity of freestream and reference area is calculated using coefficient of force=2*Normal Force/(Density*(Freestream Velocity^2)*Area). To calculate Doty and Rasmussen - normal-force coefficient , you need Normal Force (Fn), Density (ρ), Freestream Velocity (V) and Area (A). With our tool, you need to enter the respective value for Normal Force, Density, Freestream Velocity and Area 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 coefficient of force?
In this formula, coefficient of force uses Normal Force, Density, Freestream Velocity and Area. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • coefficient of force=Normal Force/(Dynamic Pressure*Area)
  • coefficient of force=Force/(Dynamic Pressure*Area)
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