Compressible Nozzle
by Mobile Education by Nil
๐๏ธ Education
Version 50+ ๐พ 471 Kb
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Updated Eligible if bought after 7/2/2016.
Learn
Calculate Convergent Divergent Nozzle thrust, mass flow rate and its condition
Features Compressible Nozzle
1.
Solves 1-D Compressible flow in Convergent Divergent Nozzle2.
Get mode of operation- Check whether existing nozzle is Subsonic Nozzle, Normal Shock exist in Nozzle, Under-expanded or Over-expanded Nozzle, under specified operating conditions.
Compute Thrust, Exit Velocity, Exit Temperature and Mass Flow rate.3.
Optimization of Nozzle - Design Nozzle for given Area ration or Pressure ratio.
Find optimum expansion conditions for given Area ratio or Pressure ratio.
Compute Optimized Nozzle performance like Thrust, Exit Velocity, Exit Temperature and Mass Flow rate.4.
Plot graphs of variations of Mach No, Pressure and Temperature in Nozzle.
5.
A tool for Students and Professionals in Rocket Propulsion design, also Aerospace and Aerodynamics geeks.Before giving negative rating, Please mail me bugs or crashes, will try to fix as early as possible.Added plotting of variations of Mach No, Pressure and Temperature changes in Nozzle.
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What Our Users Say
Don't just take our word for it. Here's what our users have to say about our Android app.
"Amazing app. Simple and precise. It helped me a lot in the beginning of my studies."
Alexandre Guitchkine
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Available for Android 8.0 and above