Momentum of Ambient Air Solution

STEP 0: Pre-Calculation Summary
Formula Used
Momentum of Ambient Air = Mass Flow Rate*Flight Speed
M = ma*V
This formula uses 3 Variables
Variables Used
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.
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.
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
Mass Flow Rate: 3.5 Kilogram per Second --> 3.5 Kilogram 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
M = ma*V --> 3.5*111
Evaluating ... ...
M = 388.5
STEP 3: Convert Result to Output's Unit
388.5 Kilogram Meter per Second --> No Conversion Required
FINAL ANSWER
388.5 Kilogram Meter per Second <-- Momentum of Ambient Air
(Calculation completed in 00.004 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

Momentum of Ambient Air Formula

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

What is ambient air?

Ambient air quality criteria, or standards, are concentrations of pollutants in the air, and typically refer to outdoor air. The criteria are specified for a variety of reasons including for the protection of human health, buildings, crops, vegetation, ecosystems, as well as for planning and other purposes.

How to Calculate Momentum of Ambient Air?

Momentum of Ambient Air calculator uses Momentum of Ambient Air = Mass Flow Rate*Flight Speed to calculate the Momentum of Ambient Air, Momentum of ambient air formula is defined as the momentum drag due to the momentum of the air passing into the engine relative to the aircraft velocity. Momentum of Ambient Air is denoted by M symbol.

How to calculate Momentum of Ambient Air using this online calculator? To use this online calculator for Momentum of Ambient Air, enter Mass Flow Rate (ma) & Flight Speed (V) and hit the calculate button. Here is how the Momentum of Ambient Air calculation can be explained with given input values -> 388.5 = 3.5*111.

FAQ

What is Momentum of Ambient Air?
Momentum of ambient air formula is defined as the momentum drag due to the momentum of the air passing into the engine relative to the aircraft velocity and is represented as M = ma*V or Momentum of Ambient Air = Mass Flow Rate*Flight Speed. Mass Flow Rate represents the amount of mass passing through a system per unit of time & Flight Speed refers to the velocity at which an aircraft moves through the air.
How to calculate Momentum of Ambient Air?
Momentum of ambient air formula is defined as the momentum drag due to the momentum of the air passing into the engine relative to the aircraft velocity is calculated using Momentum of Ambient Air = Mass Flow Rate*Flight Speed. To calculate Momentum of Ambient Air, you need Mass Flow Rate (ma) & Flight Speed (V). With our tool, you need to enter the respective value for Mass Flow Rate & Flight Speed 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!