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feat: add compressible gas dynamics, isentropic nozzle sizing, and normal shock mechanics - #4
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…normal shock mechanics Introduce verified compressible gas dynamics equations: - Stagnation temperature (T0/T) and density (rho0/rho) ratios - Isentropic nozzle area ratio (A/A*) for supersonic and subsonic regimes - Normal shock Rankine-Hugoniot relations: downstream Mach M2, static pressure jump P2/P1, and total pressure loss P02/P01 - Prandtl-Meyer supersonic expansion angle nu(M) - REST API endpoints in /fluids/compressible/ - Model Context Protocol (MCP) tool registrations: openeng_compressible_isentropic and openeng_normal_shock - Comprehensive pytest test suite with 7 new analytical verification tests Co-authored-by: Claude <noreply@anthropic.com>
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Summary of Changes
tests/test_compressible.py, 100% passing across 52 total tests.Co-authored-by: Claude noreply@anthropic.com