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
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11 Other formulas that you can solve using the same Inputs

Allowable Compression Stress when Slenderness Ratio is less than Cc
allowable compression stress=(1-((Slenderness Ratio^2)/(2*Value of Cc^2)))/((5/3)+(3*Slenderness Ratio/(8*Value of Cc))-((Slenderness Ratio^3)/(8*(Value of Cc^3))))*minimum specified yield stress of steel GO
Safety Factor for Allowable Compressive Stress
Safety factor=5/3+0.375*(Slenderness Ratio/Slenderness ratio for separation)-(0.125*(Slenderness Ratio/Slenderness ratio for separation)^3) GO
Maximum Pressure coefficient
The maximum pressure coefficient=(Total pressure-Pressure)/(0.5*Density*(Freestream Velocity)^2) GO
Allowable Compression Stress when Slenderness Ratio is Greater than Cc
allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2)) GO
Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO
Weight of aircraft for given required power
Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient) GO
Power required for given aerodynamic coefficients
Power=Weight*Freestream Velocity*Drag Coefficient/lift coefficient GO
Power required for given required thrust
Power=Freestream Velocity*Thrust of an aircraft GO
Thrust required for given required power
Thrust of an aircraft=Power/Freestream Velocity GO
Power required for given total drag
Power=Drag Force*Freestream Velocity GO
Total drag for given required power
Drag Force=Power/Freestream Velocity GO

1 Other formulas that calculate the same Output

Non dimensional Velocity disturbance in y direction in hypersonic flow
Non dimensional disturbance y velocity=(2/(Specific Heat Ratio+1))*(1-(1/Hypersonic similarity parameter^2)) GO

Non dimensional Change in hypersonic disturbance velocity in y direction Formula

Non dimensional disturbance y velocity=Change in velocity for hypersonic flow y direction/(Freestream Velocity*Slenderness Ratio)
v-'=v'/(V<sub>∞</sub>*λ )
More formulas
Change in velocity for hypersonic flow in x direction GO
Similarity constant equation with slenderness ratio GO
Density ratio with similarity constant having slenderness ratio GO
Non dimensional Change in hypersonic disturbance velocity in x 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
Doty and Rasmussen - normal-force coefficient 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 slenderness ratio?

Since the configuration under consideration is slender, the slope at any point is of the order of ratio of length to diameter of the body.

How to Calculate Non dimensional Change in hypersonic disturbance velocity in y direction?

Non dimensional Change in hypersonic disturbance velocity in y direction calculator uses Non dimensional disturbance y velocity=Change in velocity for hypersonic flow y direction/(Freestream Velocity*Slenderness Ratio) to calculate the Non dimensional disturbance y velocity, Non dimensional Change in hypersonic disturbance velocity in y direction formula is defined as ratio of small disturbance change in hypersonic velocity to product of free stream velocity and square of slenderness ratio. Non dimensional disturbance y velocity and is denoted by v-' symbol.

How to calculate Non dimensional Change in hypersonic disturbance velocity in y direction using this online calculator? To use this online calculator for Non dimensional Change in hypersonic disturbance velocity in y direction, enter Change in velocity for hypersonic flow y direction (v'), Freestream Velocity (V) and Slenderness Ratio (λ ) and hit the calculate button. Here is how the Non dimensional Change in hypersonic disturbance velocity in y direction calculation can be explained with given input values -> 0.0002 = 1/(100*50).

FAQ

What is Non dimensional Change in hypersonic disturbance velocity in y direction?
Non dimensional Change in hypersonic disturbance velocity in y direction formula is defined as ratio of small disturbance change in hypersonic velocity to product of free stream velocity and square of slenderness ratio and is represented as v-'=v'/(V*λ ) or Non dimensional disturbance y velocity=Change in velocity for hypersonic flow y direction/(Freestream Velocity*Slenderness Ratio). Change in velocity for hypersonic flow y direction but change is same the speed of fluid, 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 Slenderness ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
How to calculate Non dimensional Change in hypersonic disturbance velocity in y direction?
Non dimensional Change in hypersonic disturbance velocity in y direction formula is defined as ratio of small disturbance change in hypersonic velocity to product of free stream velocity and square of slenderness ratio is calculated using Non dimensional disturbance y velocity=Change in velocity for hypersonic flow y direction/(Freestream Velocity*Slenderness Ratio). To calculate Non dimensional Change in hypersonic disturbance velocity in y direction, you need Change in velocity for hypersonic flow y direction (v'), Freestream Velocity (V) and Slenderness Ratio (λ ). With our tool, you need to enter the respective value for Change in velocity for hypersonic flow y direction, Freestream Velocity and Slenderness Ratio 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 Non dimensional disturbance y velocity?
In this formula, Non dimensional disturbance y velocity uses Change in velocity for hypersonic flow y direction, Freestream Velocity and Slenderness Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Non dimensional disturbance y velocity=(2/(Specific Heat Ratio+1))*(1-(1/Hypersonic similarity parameter^2))
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