1 Validation map

This document records how physical claims in the theory track are checked. Each row names the claim, the independent reference it is compared against (an analytic relation, an equilibrium calculation, or a published case), and the test or example that runs the comparison. The tables are grouped by mean flow, thermochemistry, and acoustics with its inverse; where no check exists, the gap is marked openly rather than left unstated. Broader consistency evidence and named literature cases appear in verification and benchmarks.

The test names are the routines in the codebase and can be run as written.

1.1 Mean-flow claims

Claim Reference Check
Density recovery exists and is unique for any flow state with p, h_t > 0 analytic monotonicity of F(\varrho) test_real_root_matches_brentq, test_round_trip_physical_state
The recovered state is direction-independent where it must be p_t, T_t depend on M^2 test_round_trip_physical_state
An isentropic area change reproduces the classical jump analytic compressible-flow relations test_subsonic_nozzle_matches_isentropic
A sudden expansion loses the Borda–Carnot total pressure momentum balance test_expansion_unaffected_by_cc
A sudden contraction loss follows K_c = (1/C_c - 1)^2 vena-contracta model test_contraction_loss_matches_Kc, test_contraction_lossless_default_conserves_pt
Element residuals are invariant to an edge-arrow flip direction-convention algebra test_edge_direction_invariance
A long chain converges from exactly zero flow continuation well-posedness test_long_serial_chain_cold_start
A pressure-driven quiescent network converges artificial-resistance continuation test_quiescent_cold_start_converges
A symmetric branching network resolves its split Levenberg–Marquardt damping test_many_parallel_branches_converge
Choking saturates the mass flow at the sonic value critical mass flux test_choked_nozzle_saturates_mass_flow
The critical pressure ratio is the knee of the operating map p^\ast/p_t \approx 0.528 test_critical_pressure_ratio_is_the_knee
A choked orifice discharge detaches its exit pressure upward underexpanded discharge test_choked_nozzle_outlet_critical_mass_flux

1.2 Thermochemistry claims

Claim Reference Check
The equilibrium engine matches an independent equilibrium solver Cantera oracle (needs a Cantera + numba env) test_cantera_validation; public/solver packings agree via test_public_and_solver_paths_agree, test_frozen_from_xi_matches_properties
The kinetic-energy-coupled reacting state is exact equilibrium oracle at the KE-coupled enthalpy test_ke_burnt_static_matches_oracle
A transported passive scalar mixes as the mass-weighted donor convex-combination mixing test_passive_tracer_mixes_mass_weighted
A passive scalar does not perturb the mean flow scalar-registry squareness test_passive_tracer_does_not_perturb_mean_flow
A carried scalar stays realizable in [0,1] convexity of the donor mix test_passive_tracer_realizable
The marker gate selects the frozen/burnt closure and self-corrects bimodal-marker convergence test_auto_reacting_network_is_marker_gated, test_marker_self_corrects_any_seed
The marker-blended mean flow matches the hard closure frozen/equilibrium limits test_mean_flow_matches_hard_closure

1.3 Acoustic and identification claims

Claim Reference Check
The operator reduces to the base Jacobian at zero frequency (passive) \mathbf{A}(0) = \overline{\mathbf{J}} test_zero_frequency_operator_equals_jacobian
A duct carries the lossless propagation phase e^{-\mathrm{i}\omega\tau_+} test_meanflow_duct_tau_plus_phase, test_duct_scattering_is_lossless_phase
A cavity stamps the finite-volume compliance C = V/\overline{\varrho}\,\overline{c}^{\,2} test_cavity_storage_is_the_compliance
A choked-nozzle outlet reflects with the Marble–Candel coefficient compact-nozzle reflection + entropy coupling test_choked_nozzle_outlet_marble_candel
The characteristic maps are exact and invertible linearized state definitions test_characteristic_maps_are_inverse, test_characteristic_amplitude_relations
Transfer and scattering matrices round-trip, and across flavors closed-form conversions test_transfer_scattering_round_trip, test_flavor_round_trip
An n\tau flame drives a self-excited instability analytic dispersion root test_n_tau_flame_drives_self_excited_instability
The modal frequency and growth rate of a published combustor are reproduced OSCILOS (Li et al. 2017) on the EM2C combustor (Palies et al. 2011) test_dominant_mode_matches_oscilos, test_mean_flow_matches_the_reported_operating_point
A shed entropy wave is inert at a pressure-release outlet no entropy-to-acoustic conversion without acceleration test_the_entropy_wave_is_a_spectator_at_an_open_end
The acoustic and intrinsic modes of a published combustor are reproduced and told apart network analysis of the BRS rig (Emmert et al. 2017; Komarek and Polifke 2010), published eigenvalues read from vector figures test_three_dominant_modes_match_the_published_frequencies, test_the_robust_growth_rates_match_the_published_values, test_the_passive_network_matches_the_published_acoustic_modes, test_the_flame_adds_one_mode_that_the_passive_network_does_not_have
The pure intrinsic system solves the reference’s dispersion relation, as a network and as a scalar anechoic burner-and-flame system, with the FTF normalization bridge \alpha_2 test_the_pure_ita_network_matches_the_dispersion_relation, test_the_pure_ita_relation_needs_the_normalization_bridge
An intrinsic mode grows when the outlet reflection that damps it is removed reflection sweep to the published anechoic endpoint test_reducing_the_outlet_reflection_destabilizes_the_intrinsic_mode, test_the_anechoic_outlet_endpoint_matches_the_published_track
A passive heat-addition jump keeps velocity continuity under the isentropic reduction zero-Mach limit of a compact heat source test_passive_temperature_jump_keeps_the_zero_mach_velocity_continuity
A sampled impulse response is entire, so it continues to complex frequency exactly finite sum of exponentials test_fir_is_entire_and_matches_its_definition_off_the_real_axis, test_fir_single_spike_is_an_n_tau
The eigensolver’s mode count is certified complete argument-principle winding test_eigenmodes_certified_count_matches
An eigenvalue-free region yields no modes, whatever the band argument-principle winding as the Beyn rank test_beyn_moment_rank_is_ambiguous_on_an_empty_contour, test_no_modes_survive_an_eigenvalue_free_region, test_eigenmodes_are_insensitive_to_the_band_edge
A mode is told from an arbitrary frequency on an ill-conditioned operator residual on the equilibrated \mathbf{D}_r\mathbf{A}\mathbf{D}_c test_equilibrated_residual_separates_a_mode_from_an_arbitrary_point
The search sub-contours cover the region they certify elliptical tiling geometry test_subcontours_cover_the_counted_region
The growth-rate sign matches the boundary energy budget Myers acoustic energy test_boundary_power_sign_matches_growth_every_mode
The Nyquist count agrees with the eigensolver matrix-determinant lemma test_unstable_count_matches_eigenmodes
A de-embedded element reproduces its measured response Woodbury identity test_identify_transfer_matrix_cascade, test_identify_single_input_ftf
The isentropic analysis omits indirect noise (as documented) entropy-to-acoustic coupling test_isentropic_analysis_misses_the_indirect_noise

1.4 Coverage remarks

The entries above name one check per claim, not every check that backs it: many claims are tested several times, and the complete list lives in the tests themselves; this table is only a guide. The items left open in limitations (finite-rate chemistry, supersonic internal flow, and the compositional-noise gap at analytic terminal closures) are deliberately omitted here, because they mark what the present version does not yet cover or only approximates; where a partial check exists (for example a warning when compositional noise is dropped at a closure), it is noted in the limitations document, not counted as a proven result.

Basic consistency checks that support many of these entries are gathered in verification; the named literature cases and their quantitative agreement appear in benchmarks.

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References

Emmert, Thomas, Sebastian Bomberg, Stefan Jaensch, and Wolfgang Polifke. 2017. “Acoustic and Intrinsic Thermoacoustic Modes of a Premixed Combustor.” Proceedings of the Combustion Institute 36 (3): 3835–42. https://doi.org/10.1016/j.proci.2016.08.002.
Komarek, Thomas, and Wolfgang Polifke. 2010. “Impact of Swirl Fluctuations on the Flame Response of a Perfectly Premixed Swirl Burner.” Journal of Engineering for Gas Turbines and Power 132 (6): 061503. https://doi.org/10.1115/1.4000127.
Li, Jingxuan, Dong Yang, Charles Luzzato, and Aimee S. Morgans. 2017. Open Source Combustion Instability Low Order Simulator (OSCILOS–Long) Technical Report. Department of Mechanical Engineering, Imperial College London. https://www.oscilos.com.
Palies, Paul, Daniel Durox, Thierry Schuller, and Sébastien Candel. 2011. “Nonlinear Combustion Instability Analysis Based on the Flame Describing Function Applied to Turbulent Premixed Swirling Flames.” Combustion and Flame 158 (10): 1980–91. https://doi.org/10.1016/j.combustflame.2011.02.012.