Mobile Education by Nil Apps

Normal Shock Relations can be obtained usingthis app. The flow variable values across Normal Shock wave aregenerally tabulated in Text Books. In place of Tables one can usethis handy app.Select any known variable from list, M1, P2/P1, T2/T1, M2,rho2/rho1, Po2/Po1, and Po2/P1, input its value and user cancalculate remaining variable values. The Indices 1 and 2 are forbefore shock and after shock respectively.

Isentropic Relations,Normal Shock,Oblique Shock,Vortex LatticeMethod,Pitot Tube

Calculate Convergent Divergent Nozzle thrust, mass flow rate andits condition

1. Compressible flow in ConvergentDivergentNozzle2. Get mode of operation under specified operatingconditions-Whether nozzle is Subsonic Nozzle, Normal Shock exist inNozzle,location of Shock, Under-expanded or Over-expanded Nozzle.ComputeThrust, Exit Velocity, Exit Temperature and Mass Flowrate.3. Optimization of Nozzle - Optimize Nozzle keeping fixedArearation or Pressure ratio. Find optimum expansion conditionsforgiven Area ratio or Pressure ratio. Compute OptimizedNozzleperformance like Thrust, Exit Velocity, Exit Temperature andMassFlow rate.4. Paid version contains- Plotting Graph of Flow VariableslikeMach No, Pressure, Temperature through nozzle.5. A tool for Students and Professionals in RocketPropulsiondesign and Aerospace Engineering. Check first handnozzleperformance using this tool before going for complexCFDsimulations.Before giving negative rating, Please mail me bugs or crashes,willtry to fix as early as possible.Consider buying ad free version if you like thisThanks

Calculator for - Isentropic relations, Normal Shock, Oblique Shock,etc