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Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator

Easily calculate and compute afterburner thrust augmentation ratio & temperature rise calculator with accurate equations, live formulas, and expert guidance.

Military maximum unaugmented dry thrust.

Pre-afterburner exhaust gas entry temperature.

Maximum augmented reheat combustion temperature.

Dry military rating specific fuel consumption.

Calculated Result
1.49

Augmentation Ratio

Augmentation Ratio

1.49

Thrust Augmentation Ratio

1.49

Wet Augmented Thrust K N

96.6

Thrust Increase Percentage

48.7

Estimated Wet Tsfc Kg Per Knh

248.9

1.49

Calculation Breakdown

  1. Applied FormulaCalculates reheat thrust augmentation ratio, wet augmented thrust, and exponential specific fuel consumption surge in military afterburning turbofans.\frac{F_{wet}}{F_{dry}} = \sqrt{\frac{T_{t7}}{T_{t4}}}, \quad \Delta F = F_{dry} \left(\sqrt{\frac{T_{t7}}{T_{t4}}} - 1\right)

Afterburner Augmentation Metric Output

Interactive visualization based on your current inputs

Calculated Value
0.00.40.71.11.5Augmentation Ratio

What Is the Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator?

This tool computes afterburner thrust augmentation ratio & temperature rise calculator with high precision arithmetic.

How Does the Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator Work?

Calculates reheat thrust augmentation ratio, wet augmented thrust, and exponential specific fuel consumption surge in military afterburning turbofans.

Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

FwetFdry=Tt7Tt4,ΔF=Fdry(Tt7Tt4−1)\frac{F_{wet}}{F_{dry}} = \sqrt{\frac{T_{t7}}{T_{t4}}}, \quad \Delta F = F_{dry} \left(\sqrt{\frac{T_{t7}}{T_{t4}}} - 1\right)

Calculates reheat thrust augmentation ratio, wet augmented thrust, and exponential specific fuel consumption surge in military afterburning turbofans.

How to Use the Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator

  1. Enter your parameters into the designated input fields to calculate the result immediately.

Step-by-Step Example Calculation

Afterburner Thrust Augmentation Ratio & Temperature Rise Calculator Example

Input Values:

dryThrustKN:65.0
turbineExitGasTempT4K:950.0
afterburnerFlameTempT7K:2100.0
dryTSFCKgPerKnh:82.0
Worked Steps: Sample evaluation based on standard reference conditions.

Understanding Your Result

The calculated primary figure indicates the optimal or required Augmentation Ratio.

Factors That Affect the Result

  • Measurement tolerances, operational variance, and real-world conditions.

When Should You Use This Calculator?

  • Everyday budgeting, technical homework, professional estimation, and household projects.

Assumptions & Limitations

  • Assumes standard atmospheric or environmental parameters unless specified.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Double-precision IEEE 754 arithmetic with validated empirical constants.

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