Mass Flow given Momentum in Ambient Air Solution

STEP 0: Pre-Calculation Summary
Formula Used
Mass Flow Rate = Momentum of Ambient Air/Flight Speed
ma = M/V
This formula uses 3 Variables
Variables Used
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.
Momentum of Ambient Air - (Measured in Kilogram Meter per Second) - Momentum of Ambient Air refers to the linear motion possessed by the surrounding air in its natural state.
Flight Speed - (Measured in Meter per Second) - Flight Speed refers to the velocity at which an aircraft moves through the air.
STEP 1: Convert Input(s) to Base Unit
Momentum of Ambient Air: 388.5 Kilogram Meter per Second --> 388.5 Kilogram Meter per Second No Conversion Required
Flight Speed: 111 Meter per Second --> 111 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
ma = M/V --> 388.5/111
Evaluating ... ...
ma = 3.5
STEP 3: Convert Result to Output's Unit
3.5 Kilogram per Second --> No Conversion Required
FINAL ANSWER
3.5 Kilogram per Second <-- Mass Flow Rate
(Calculation completed in 00.020 seconds)

Credits

Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
Kartikay Pandit has verified this Calculator and 400+ more calculators!

21 Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy
Go Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine)))
Momentum Thrust
Go Ideal Thrust = Mass Flow Rate*((1+Fuel Air Ratio)*Exit Velocity-Flight Speed)
Thrust power
Go Thrust Power = Mass Flow Rate*Flight Speed*(Exit Velocity-Flight Speed)
Ideal Thrust given Effective Speed Ratio
Go Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)
Thrust given aircraft forward speed, velocity of exhaust
Go Ideal Thrust = Mass Flow Rate*(Exit Velocity-Flight Speed)
Mass Flow Rate given Ideal Thrust
Go Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed)
Ideal Thrust of Jet Engine
Go Ideal Thrust = Mass Flow Rate*(Exit Velocity-Flight Speed)
Velocity after Expansion given Ideal Thrust
Go Exit Velocity = Ideal Thrust/Mass Flow Rate+Flight Speed
Flight Speed given Ideal Thrust
Go Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate
Thrust specific fuel consumption
Go Thrust-Specific Fuel Consumption = (3600*Fuel Air Ratio)/Specific Thrust
Thrust power specific fuel consumption
Go Thrust Power Specific Fuel Consumption = Fuel Flow Rate/Thrust Power
Gross Thrust Coefficient
Go Gross Thrust Coefficient = Gross Thrust/Ideal Gross Thrust
Specific Thrust given Effective Speed Ratio
Go Specific Thrust = Exit Velocity*(1-Effective Speed Ratio)
Flight Speed given Momentum of Ambient Air
Go Flight Speed = Momentum of Ambient Air/Mass Flow Rate
Mass Flow given Momentum in Ambient Air
Go Mass Flow Rate = Momentum of Ambient Air/Flight Speed
Momentum of Ambient Air
Go Momentum of Ambient Air = Mass Flow Rate*Flight Speed
Specific thrust
Go Specific Thrust = Exit Velocity-Flight Speed
Gross thrust
Go Gross Thrust = Mass Flow Rate*Exit Velocity
Mass Flow Rate given Ram Drag and Flight Speed
Go Mass Flow Rate = Ram Drag/Flight Speed
Flight Speed given Ram Drag and Mass Flow Rate
Go Flight Speed = Ram Drag/Mass Flow Rate
Ram drag
Go Ram Drag = Mass Flow Rate*Flight Speed

Mass Flow given Momentum in Ambient Air Formula

Mass Flow Rate = Momentum of Ambient Air/Flight Speed
ma = M/V

what is ambient air?

Ambient air quality criteria, or standards, are concentrations of pollutants in the air, and typically refer to outdoor air.

How to Calculate Mass Flow given Momentum in Ambient Air?

Mass Flow given Momentum in Ambient Air calculator uses Mass Flow Rate = Momentum of Ambient Air/Flight Speed to calculate the Mass Flow Rate, Mass Flow given Momentum in Ambient Air formulas is defined as ratio of momentum of ambient air to the flight velocity. Mass Flow Rate is denoted by ma symbol.

How to calculate Mass Flow given Momentum in Ambient Air using this online calculator? To use this online calculator for Mass Flow given Momentum in Ambient Air, enter Momentum of Ambient Air (M) & Flight Speed (V) and hit the calculate button. Here is how the Mass Flow given Momentum in Ambient Air calculation can be explained with given input values -> 0.011081 = 388.5/111.

FAQ

What is Mass Flow given Momentum in Ambient Air?
Mass Flow given Momentum in Ambient Air formulas is defined as ratio of momentum of ambient air to the flight velocity and is represented as ma = M/V or Mass Flow Rate = Momentum of Ambient Air/Flight Speed. Momentum of Ambient Air refers to the linear motion possessed by the surrounding air in its natural state & Flight Speed refers to the velocity at which an aircraft moves through the air.
How to calculate Mass Flow given Momentum in Ambient Air?
Mass Flow given Momentum in Ambient Air formulas is defined as ratio of momentum of ambient air to the flight velocity is calculated using Mass Flow Rate = Momentum of Ambient Air/Flight Speed. To calculate Mass Flow given Momentum in Ambient Air, you need Momentum of Ambient Air (M) & Flight Speed (V). With our tool, you need to enter the respective value for Momentum of Ambient Air & Flight Speed 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 Mass Flow Rate?
In this formula, Mass Flow Rate uses Momentum of Ambient Air & Flight Speed. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Mass Flow Rate = Ram Drag/Flight Speed
  • Mass Flow Rate = Ideal Thrust/(Exit Velocity-Flight Speed)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!