Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Calorie Burn Rate
Calorie Burn Rate=(Weight*Sleeping*Time)+(Weight*Watching TV*Time)+(Weight*Typing Writing Desk Work*Time)+(Weight*Walking Very Slow 1.7 Mph)+(Weight*Walking 2.5 mph*Time)+(Weight*Bicycling Very Slow 50 Watts*Time)+(Weight*Walking 3 Mph*Time)+(Weight*Calisthenics Home Exercises*Time)+(Weight*Walking 3.4 Mph*Time)+(Weight*Bicycling Stationary*Time)+(Weight*Jogging *Time)+(Weight*Heavy Calisthenics*Time)+(Weight*Running Jogging In Place*Time)+(Weight*Rope Jumping*Time) GO
Heart Rate Based Calorie Burn For Male
Heart Rate Based Calorie Burn For Male=((-55.0969+(0.6309*Heart Rate)+(0.1988*Weight)+(0.2017*Age))/4.184)*60*Time GO
Maximum Pressure coefficient
The maximum pressure coefficient=(Total pressure-Pressure)/(0.5*Density*(Freestream Velocity)^2) GO
Non-dimensional pressure
Non-dimensionalized Pressure=Pressure/(Density*(Freestream Velocity)^2) 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
Heat generated through resistance
Heat Rate=Electric Current^2*Resistance*Time 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

Distance from tip of the leading edge to the base Formula

Distance from X-axis=Freestream Velocity*Time
y=V<sub>∞</sub>*t
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 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
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

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 the leading edge to the base?

Distance from tip of the leading edge to the base calculator uses Distance from X-axis=Freestream Velocity*Time to calculate the Distance from X-axis, The Distance from tip of the leading edge to the base formula is defined as the ratio of time to the ratio of length and the freestream velocity. Distance from X-axis and is denoted by y symbol.

How to calculate Distance from tip of the leading edge to the base using this online calculator? To use this online calculator for Distance from tip of the leading edge to the base, enter Freestream Velocity (V) and Time (t) and hit the calculate button. Here is how the Distance from tip of the leading edge to the base calculation can be explained with given input values -> 1.440E+9 = 100*14400.

FAQ

What is Distance from tip of the leading edge to the base?
The Distance from tip of the leading edge to the base formula is defined as the ratio of time to the ratio of length and the freestream velocity and is represented as y=V*t or Distance from X-axis=Freestream Velocity*Time. 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 Time can be defined as the ongoing and continuous sequence of events that occur in succession, from the past through the present to the future.
How to calculate Distance from tip of the leading edge to the base?
The Distance from tip of the leading edge to the 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*Time. To calculate Distance from tip of the leading edge to the base, you need Freestream Velocity (V) and Time (t). With our tool, you need to enter the respective value for Freestream Velocity and Time 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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