Distance from Tip of Leading Edge to Base Calculator

✖Freestream Velocity for Blast Wave 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.ⓘ Freestream Velocity for Blast Wave [U_{∞ bw}]			+10% -10%
✖Total Time Taken is the total time taken by the body to cover that space.ⓘ Total Time Taken [t]			+10% -10%

✖Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.ⓘ Distance from Tip of Leading Edge to Base [y]

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Formula

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Distance from Tip of Leading Edge to Base

Formula

`"y" = "U"_{"∞ bw"}*"t"`

Example

`"0.04096m"="0.0512m/s"*"0.8s"`

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Download Hypersonic Flow and Disturbances Formulas PDF

Distance from Tip of Leading Edge to Base Solution

STEP 0: Pre-Calculation Summary

Formula Used

Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken
y = U_{∞ bw}*t
This formula uses 3 Variables

Variables Used

Distance from X-Axis - (Measured in Meter) - Distance from X-Axis is defined as the distance from the point where stress is to be computed to XX axis.
Freestream Velocity for Blast Wave - (Measured in Meter per Second) - Freestream Velocity for Blast Wave 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.
Total Time Taken - (Measured in Second) - Total Time Taken is the total time taken by the body to cover that space.

STEP 1: Convert Input(s) to Base Unit

Freestream Velocity for Blast Wave: 0.0512 Meter per Second --> 0.0512 Meter per Second No Conversion Required
Total Time Taken: 0.8 Second --> 0.8 Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

y = U_{∞ bw}*t --> 0.0512*0.8

Evaluating ... ...

y = 0.04096

STEP 3: Convert Result to Output's Unit

0.04096 Meter --> No Conversion Required

FINAL ANSWER

0.04096 Meter <-- Distance from X-Axis

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

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< 17 Hypersonic Flow and Disturbances Calculators

Inverse of Density for Hypersonic Flow using Mach Number

Go Inverse of Density = (2+(Specific Heat Ratio-1)*Mach Number^2*sin(Deflection Angle)^2)/(2+(Specific Heat Ratio+1)*Mach Number^2*sin(Deflection Angle)^2)

Coefficient of Pressure with Slenderness Ratio and Similarity Constant

Go Pressure Coefficient = (2*Slenderness Ratio^2)/(Specific Heat Ratio*Hypersonic Similarity Parameter^2)*(Specific Heat Ratio*Hypersonic Similarity Parameter^2*Non Dimensionalized Pressure-1)

Coefficient of Pressure with Slenderness Ratio

Go Pressure Coefficient = 2/Specific Heat Ratio*Mach Number^2*(Non Dimensionalized Pressure*Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2-1)

Non Dimensional Pressure Equation with Slenderness Ratio

Go Non Dimensionalized Pressure = Pressure/(Specific Heat Ratio*Mach Number^2*Slenderness Ratio^2*Free Stream Pressure)

Density Ratio with Similarity Constant having Slenderness Ratio

Go Density Ratio = ((Specific Heat Ratio+1)/(Specific Heat Ratio-1))*(1/(1+2/((Specific Heat Ratio-1)*Hypersonic Similarity Parameter^2)))

Rasmussen Closed Form Expression for Shock Wave Angle

Go Wave Angle Similarity Parameter = Hypersonic Similarity Parameter*sqrt((Specific Heat Ratio+1)/2+1/Hypersonic Similarity Parameter^2)

Non Dimensional Change in Hypersonic Disturbance Velocity in y Direction

Go Non Dimensional Disturbance Y Velocity = Change in Velocity for Hypersonic Flow y direction/(Freestream Velocity Normal*Slenderness Ratio)

Non Dimensional Change in Hypersonic Disturbance Velocity in x Direction

Go Non Dimensional Disturbance X Velocity = Change in Velocity for Hypersonic Flow/(Freestream Velocity for Blast Wave*Slenderness Ratio^2)

Doty and Rasmussen- Normal Force Coefficient

Go Coefficient of Force = 2*Normal Force/(Density of Fluid*Freestream Velocity Normal^2*Area)

Constant G used for Finding Location of Perturbed Shock

Go Perturbed Shock Location Constant = Perturbed Shock Location Constant at Normal Force/Perturbed Shock Location Constant at Drag Force

Non Dimensional Velocity Disturbance in y Direction in Hypersonic Flow

Go Non Dimensional Disturbance Y Velocity = (2/(Specific Heat Ratio+1))*(1-1/Hypersonic Similarity Parameter^2)

Non Dimensionalised Time

Go Non Dimensionalized Time = Time/(Length/Freestream Velocity Normal)

Similarity Constant Equation using Wave Angle

Go Wave Angle Similarity Parameter = Mach Number*Wave Angle*180/pi

Change in Velocity for Hypersonic Flow in X Direction

Go Change in Velocity for Hypersonic Flow = Fluid Velocity-Freestream Velocity Normal

Distance from Tip of Leading Edge to Base

Go Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken

Similarity Constant Equation with Slenderness Ratio

Go Hypersonic Similarity Parameter = Mach Number*Slenderness Ratio

Inverse of Density for Hypersonic Flow

Go Inverse of Density = 1/(Density*Wave Angle)

Distance from Tip of Leading Edge to Base Formula

Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken
y = U_{∞ bw}*t

What is hypersonic flow?

Hypersonic flows are flow fields where the fluid velocity is much larger than the velocity of propagation of small disturbances, the velocity of sound

How to Calculate Distance from Tip of Leading Edge to Base?

Distance from Tip of Leading Edge to Base calculator uses Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken to calculate the Distance from X-Axis, The Distance from tip of leading edge to base formula is defined as the ratio of time to the ratio of length and the freestream velocity. Distance from X-Axis is denoted by y symbol.

How to calculate Distance from Tip of Leading Edge to Base using this online calculator? To use this online calculator for Distance from Tip of Leading Edge to Base, enter Freestream Velocity for Blast Wave (U_{∞ bw}) & Total Time Taken (t) and hit the calculate button. Here is how the Distance from Tip of Leading Edge to Base calculation can be explained with given input values -> 40960 = 0.0512*0.8.

FAQ

What is Distance from Tip of Leading Edge to Base?

The Distance from tip of leading edge to base formula is defined as the ratio of time to the ratio of length and the freestream velocity and is represented as y = U_{∞ bw}*t or Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken. Freestream Velocity for Blast Wave 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 & Total Time Taken is the total time taken by the body to cover that space.

How to calculate Distance from Tip of Leading Edge to Base?

The Distance from tip of leading edge to base formula is defined as the ratio of time to the ratio of length and the freestream velocity is calculated using Distance from X-Axis = Freestream Velocity for Blast Wave*Total Time Taken. To calculate Distance from Tip of Leading Edge to Base, you need Freestream Velocity for Blast Wave (U_{∞ bw}) & Total Time Taken (t). With our tool, you need to enter the respective value for Freestream Velocity for Blast Wave & Total Time Taken and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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