Categories
Aerodynamics Calculator Aerospace Calculator Aircraft Design Airplane Performance Calculator Engineering Calculator Flight Mechanics Calculator General Calculator Physics Calculator Science Calculator

Total Temperature Calculator by Mohit Kudal

Total temperature is combination of the static temperature and velocity relation. Its SI unit is Kelvin.

Where T- static temperature

V- Velocity

Cp- specific heat at constant pressure

Categories
Aerodynamics Calculator Aerospace Calculator Aircraft Design Airplane Performance Calculator Engineering Calculator Flight Mechanics Calculator General Calculator Physics Calculator Science Calculator

Total pressure Calculator by Mohit Kudal

Total pressure is the combination of the static pressure and dynamic pressure. Its SI unit is N/m^2.

Where P- static pressure

ρ- density

V- velocity

Categories
Aerodynamics Calculator Aerospace Calculator Aircraft Design Airplane Performance Calculator Engineering Calculator Flight Mechanics Calculator General Calculator Physics Calculator Science Calculator

Specific Heat Ratio Calculator by Mohit Kudal

Specific heat is the ratio of specific heat at constant pressure to the specific heat at constant volume. It is also known as Isentropic expansion factor.

\gamma= \frac {C_P}{C_V}

Where Cp- specific heat at constant pressure

Cv- specific heat at constant volume

 

 

Categories
Aerodynamics Calculator Aerospace Calculator Aircraft Design Airplane Performance Calculator Engineering Calculator Flight Mechanics Calculator General Calculator Physics Calculator Science Calculator

Reynold number for a Pipe Calculator by Mohit Kudal

The Reynold number is the ratio of two forces between inertia force and viscous force. It separates the flow. It is a dimensionless quantity.

Re=ρ*V*D/μ=V*D/ν

Categories
Aerodynamics Calculator Aerospace Calculator Aircraft Design Airplane Performance Calculator Engineering Calculator Flight Mechanics Calculator General Calculator Physics Calculator Science Calculator

Mach Number Calculator by Mohit Kudal

Mach number is the ratio of velocity of object and speed of sound.

Mach number is categorized by its value:-

M<0.8 Subsonic

0.8<M<1.2 Transonic

M=1 – Sonic

M>1 Supersonic

M>5 Hypersonic