№ lp_2_3_28814
MATLAB source code defining isentropic and normal shock relations and applying iterative numerical methods to compute shock location and flow property distributions in a converging-diverging nozzle.
Document Type: MATLAB script
Subject: Compressible flow analysis
Topic: Isentropic relations, normal shock relations, linear interpolation
Application: Converging-diverging nozzle flow
Working Fluid: Air
Specific Heat Ratio (Gamma): 1.4
Input Parameters: Exit static-to-total pressure ratio; Exit area-to-throat area ratio
Output Data: Shock location; Mach number distribution; Static pressure distribution; Temperature distribution
Numerical Methods: Secant method; Linear interpolation
Generated Outputs: Graphs of Mach number, static pressure ratio, and temperature ratio versus downstream distance
Price: 8 / 10 USD
The file will be delivered to the email address provided at checkout within 12 hours.

Don’t have cryptocurrency yet?

You can still complete your purchase in a few minutes:
  1. Buy Crypto in a trusted app (Coinbase, Kraken, Cash App or any similar service).
  2. In the app, tap Send.
  3. Select network, paste our wallet address.
  4. Send the exact amount shown above.
After sending, paste your TXID (transaction ID) and your email to receive the download link. Need help? Contact support and we’ll guide you step by step.