True Aircraft Speed (Mach number) Solution

STEP 0: Pre-Calculation Summary
Formula Used
True Aircraft Speed = Speed of Sound*True Mach Number
VTAS = c*MTrue
This formula uses 3 Variables
Variables Used
True Aircraft Speed - (Measured in Meter per Hour) - True Aircraft Speed of an aircraft is the speed of the aircraft relative to the air mass through which it is flying.
Speed of Sound - (Measured in Meter per Hour) - Speed of Sound in the air is considered here and is denoted by c symbol.
True Mach Number - True Mach Number of the aircraft. Mach number is a function of temperature and true airspeed. Aircraft flight instruments operate using pressure differential to compute Mach number, not temperature.
STEP 1: Convert Input(s) to Base Unit
Speed of Sound: 47.5 Kilometer per Hour --> 47500 Meter per Hour (Check conversion ​here)
True Mach Number: 4 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
VTAS = c*MTrue --> 47500*4
Evaluating ... ...
VTAS = 190000
STEP 3: Convert Result to Output's Unit
52.7777777777778 Meter per Second -->190 Kilometer per Hour (Check conversion ​here)
FINAL ANSWER
190 Kilometer per Hour <-- True Aircraft Speed
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Mithila Muthamma PA
Coorg Institute of Technology (CIT), Coorg
Mithila Muthamma PA has created this Calculator and 2000+ more calculators!
Verifier Image
Verified by Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has verified this Calculator and 1700+ more calculators!

Aircraft Runway Length Estimation Calculators

Operating Empty Weight when Desired Take-off Weight is considered
​ LaTeX ​ Go Operating Empty Weight = Desired Takeoff Weight of Aircraft-Payload Carried-Fuel Weight to be carried
Payload carried when desired take-off weight is considered
​ LaTeX ​ Go Payload Carried = Desired Takeoff Weight of Aircraft-Operating Empty Weight-Fuel Weight to be carried
Fuel Weight to be Carried given Desired Takeoff Weight
​ LaTeX ​ Go Fuel Weight to be carried = Desired Takeoff Weight of Aircraft-Payload Carried-Operating Empty Weight
Desired Take off Weight
​ LaTeX ​ Go Desired Takeoff Weight of Aircraft = Payload Carried+Operating Empty Weight+Fuel Weight to be carried

True Aircraft Speed (Mach number) Formula

​LaTeX ​Go
True Aircraft Speed = Speed of Sound*True Mach Number
VTAS = c*MTrue

What is Maximum Structural Payload Weight ?

Maximum Structural Payload Weight (or mass) is the maximum demonstrated payload to be carried without stressing the aircraft fuselage. Maximum zero fuel weight (or mass) is the sum of the operating empty weight and the maximum structural payload weight.

What is Mach number?

The ratio between the the true air speed (TAS) and the local speed of sound (LSS). This ratio, which equals one when the TAS is equal to the LSS, is known as the Mach Number (M) and is very important in aircraft operating at high speed.

How to Calculate True Aircraft Speed (Mach number)?

True Aircraft Speed (Mach number) calculator uses True Aircraft Speed = Speed of Sound*True Mach Number to calculate the True Aircraft Speed, True Aircraft Speed (Mach number) is defined as the equivalent airspeed corrected for temperature and pressure altitude. True Aircraft Speed is denoted by VTAS symbol.

How to calculate True Aircraft Speed (Mach number) using this online calculator? To use this online calculator for True Aircraft Speed (Mach number), enter Speed of Sound (c) & True Mach Number (MTrue) and hit the calculate button. Here is how the True Aircraft Speed (Mach number) calculation can be explained with given input values -> 684 = 13.1944444444444*4.

FAQ

What is True Aircraft Speed (Mach number)?
True Aircraft Speed (Mach number) is defined as the equivalent airspeed corrected for temperature and pressure altitude and is represented as VTAS = c*MTrue or True Aircraft Speed = Speed of Sound*True Mach Number. Speed of Sound in the air is considered here and is denoted by c symbol & True Mach Number of the aircraft. Mach number is a function of temperature and true airspeed. Aircraft flight instruments operate using pressure differential to compute Mach number, not temperature.
How to calculate True Aircraft Speed (Mach number)?
True Aircraft Speed (Mach number) is defined as the equivalent airspeed corrected for temperature and pressure altitude is calculated using True Aircraft Speed = Speed of Sound*True Mach Number. To calculate True Aircraft Speed (Mach number), you need Speed of Sound (c) & True Mach Number (MTrue). With our tool, you need to enter the respective value for Speed of Sound & True Mach Number and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!