Flight Speed given Ram Drag and Mass Flow Rate Calculator

✖Ram Drag refers to the drag force experienced by a jet engine due to the impact of air at high speeds.ⓘ Ram Drag [D_ram]			+10% -10%
✖Mass Flow Rate represents the amount of mass passing through a system per unit of time.ⓘ Mass Flow Rate [m_a]			+10% -10%

✖Flight Speed refers to the velocity at which an aircraft moves through the air.ⓘ Flight Speed given Ram Drag and Mass Flow Rate [V]

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Flight Speed given Ram Drag and Mass Flow Rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Flight Speed = Ram Drag/Mass Flow Rate
V = D_ram/m_a
This formula uses 3 Variables

Variables Used

Flight Speed - (Measured in Meter per Second) - Flight Speed refers to the velocity at which an aircraft moves through the air.
Ram Drag - (Measured in Newton) - Ram Drag refers to the drag force experienced by a jet engine due to the impact of air at high speeds.
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.

STEP 1: Convert Input(s) to Base Unit

Ram Drag: 389 Newton --> 389 Newton No Conversion Required
Mass Flow Rate: 3.5 Kilogram per Second --> 3.5 Kilogram per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V = D_ram/m_a --> 389/3.5

Evaluating ... ...

V = 111.142857142857

STEP 3: Convert Result to Output's Unit

111.142857142857 Meter per Second --> No Conversion Required

FINAL ANSWER

111.142857142857 ≈ 111.1429 Meter per Second <-- Flight Speed

(Calculation completed in 00.020 seconds)

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Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

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National Institute Of Technology (NIT), Hamirpur

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< Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy

LaTeX 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)))

Thrust power

LaTeX Go Thrust Power = Mass Flow Rate*Flight Speed*(Exit Velocity-Flight Speed)

Ideal Thrust given Effective Speed Ratio

LaTeX Go Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)

Specific thrust

LaTeX Go Specific Thrust = Exit Velocity-Flight Speed

Flight Speed given Ram Drag and Mass Flow Rate Formula

LaTeX Go

Flight Speed = Ram Drag/Mass Flow Rate
V = D_ram/m_a

What is flight speed?

Flight speed of an aircraft is the airspeed sufficient to provide the lift necessary to support an airplane in level flight.

How to Calculate Flight Speed given Ram Drag and Mass Flow Rate?

Flight Speed given Ram Drag and Mass Flow Rate calculator uses Flight Speed = Ram Drag/Mass Flow Rate to calculate the Flight Speed, The Flight Speed given Ram Drag and Mass Flow Rate formula is defined as the division of ram drag value of the thrust by mass flow rate of the thrust of the turbojet. Flight Speed is denoted by V symbol.

How to calculate Flight Speed given Ram Drag and Mass Flow Rate using this online calculator? To use this online calculator for Flight Speed given Ram Drag and Mass Flow Rate, enter Ram Drag (D_ram) & Mass Flow Rate (m_a) and hit the calculate button. Here is how the Flight Speed given Ram Drag and Mass Flow Rate calculation can be explained with given input values -> 198.2857 = 389/3.5.

FAQ

What is Flight Speed given Ram Drag and Mass Flow Rate?

The Flight Speed given Ram Drag and Mass Flow Rate formula is defined as the division of ram drag value of the thrust by mass flow rate of the thrust of the turbojet and is represented as V = D_ram/m_a or Flight Speed = Ram Drag/Mass Flow Rate. Ram Drag refers to the drag force experienced by a jet engine due to the impact of air at high speeds & Mass Flow Rate represents the amount of mass passing through a system per unit of time.

How to calculate Flight Speed given Ram Drag and Mass Flow Rate?

The Flight Speed given Ram Drag and Mass Flow Rate formula is defined as the division of ram drag value of the thrust by mass flow rate of the thrust of the turbojet is calculated using Flight Speed = Ram Drag/Mass Flow Rate. To calculate Flight Speed given Ram Drag and Mass Flow Rate, you need Ram Drag (D_ram) & Mass Flow Rate (m_a). With our tool, you need to enter the respective value for Ram Drag & Mass Flow Rate 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 Flight Speed?

In this formula, Flight Speed uses Ram Drag & Mass Flow Rate. We can use 2 other way(s) to calculate the same, which is/are as follows -

Flight Speed = Momentum of Ambient Air/Mass Flow Rate
Flight Speed = Exit Velocity-Ideal Thrust/Mass Flow Rate

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