We sealed our predictions before running the experiments — across six public battery datasets. Full scorecard, including two unedited falsifications.
▲ 1 r/ScientificComputing+2 crossposts

We sealed our predictions before running the experiments — across six public battery datasets. Full scorecard, including two unedited falsifications.

TL;DR

- One data-level diagnostic workflow, applied to six battery fleets from five public sources (NASA PCoE; CALCE/UMD — the CS2 and CX2 series; MIT/Severson; Oxford; HUST). Every prediction was written down and hashed before the corresponding experiment ran — one of them with a publicly timestamped, Bitcoin-seeded protocol anyone can verify.

- Diagnosis mode: on the HUST fleet (77 cells, never touched before), we predicted an error-reduction band of [−45%, −20%] before modeling. Measured: −34.4%. Hit.

- Design mode: using only the manufacturer's spec sheet (max continuous charge current, 4A) plus Joule's law, we located the empirically best fast-charging policy in the MIT/Severson fleet within 2.2% of the measured optimum — before looking at any lifetime data.

- We also publish two clean falsifications: sealed predictions that missed. They stay in the record.

- We are not publishing the algorithm. We are publishing protocols, data sources, and verdicts.

  1. Why we pre-register everything

Battery RUL papers are full of numbers that were polished after the fact. We wanted protection against our own hindsight bias, so every experiment in this campaign follows the same rule: the prediction — with explicit numeric bands — is written to a dated, hashed document before the experiment runs. Afterward we score against the sealed document, not against our memory. Two of our sealed predictions failed. Both failures are below, unchanged.

  1. Scorecard: diagnosis mode (six fleets)

The task: predict remaining useful life (RUL) under strict fleet-level protocols (leave-one-battery-out or leave-one-batch-out, nested train-only CV for all choices, official splits where they exist). Two task modes are used, and we label them explicitly: (a) lifetime from early data — MIT only, features from cycles ≤ 100 predict the full cycle life; (b) online RUL — all other fleets, at each cycle the model uses only data up to that cycle (no future information). Baseline ("naive") uses cycle count + current capacity only; the treatment adds an early-life feature set selected by the diagnostic. Leverage = (naive − treated) / naive, computed against the deployed treated configuration in every row.

Fleet Protocol Naive RMSE Treated RMSE (deployed) Leverage

NASA Li-ion (B0005/6/18) nested LOBO (b) 11.34 7.03 −38.0%

MIT/Severson (124 cells) official split (a) 248.8 (primary) / 481.4 (secondary) 128.7 (primary) / 189.9 (secondary) −48.3% / −60.6%

CALCE CS2 (4 cells) LOBO (b) 10.82 10.82 (suite declined features) 0% — called in advance

Oxford Degradation (8 cells) nested LOBO (b) 76.5 56.9 (deployed); 51.4 best subset −25.6% (subset: −32.8%)

HUST (77 cells, 10 batches) leave-one-batch-out (b) 58.7 38.5 −34.4%

CALCE CX2 (7 prismatic cells) nested LOBO (b) 81.2 63.4 −21.9% (see §3b)

Oxford note: the deployed treated model (56.9 RMSE, −25.6%) is the number the sealed band prediction was scored against in §5 — the post-hoc best subset (51.4, −32.8%) is reported for completeness but is not the deployed figure.

The CALCE row deserves explanation: before modeling, our diagnostic said this fleet has "nothing to repair," so the suite declined to add features and deployed the baseline. It was right — adding features made things worse (23.68 vs 10.82). Knowing when not to act is half the value of a diagnostic.

2b. Benchmark position — same-protocol comparisons only

We compare numbers only where the protocol matches, and we cite the source for every literature figure. RMSE in cycles; primary / secondary test sets as defined in each source.

MIT/Severson official split (41 train / 43 primary / 40 secondary), EOL = capacity < 0.88 Ah, features from cycles ≤ 100 only:

Model Primary Secondary

Severson et al. — discharge model (Table 1) 91 173

Severson et al. — variance model (Table 1) 138 196

Severson et al. — full model (Table 1) 118 214

BatteryML (Microsoft, ICLR 2024) — MATR-1/2 dummy baseline 398 510

Ours (diagnostic-selected features, ridge) 128.7 189.9

Position: we beat the variance and full models on the secondary set and the variance model on the primary set; the discharge-curve model (91/173) remains ahead of us. Our dummy-baseline check (392.8 / 491.8) lands within 1.3% (primary) and 3.6% (secondary) of BatteryML's published reproduction (398 / 510), which independently anchors that our split and labels match the literature pipeline.

NASA Li-ion: no comparison claimed. Most published NASA numbers train and test on cycles of the same battery; ours is leave-one-battery-out across different cells. Those protocols measure different things, so we do not put the numbers side by side.

HUST / Oxford / CALCE: run under our own strict fleet-level protocols (below); we are not aware of published results under identical protocols, so we report absolute numbers only.

We deliberately make no "SOTA" or "record" claims anywhere in this post. Every number above comes from our own runs; literature figures are quoted with their sources.

  1. The part we're most proud of: predicting the leverage itself

Across the first five fleets we noticed the leverage is not random — it tracks how heterogeneous the fleet is. We formalized this with two dispersion indices computed from early-life data only [we are keeping the exact definitions unpublished], and a band rule that maps index values to expected leverage. Then we tested it on a fleet we had never touched:

&gt; Sealed prediction (before any HUST modeling): "Both indices fall in the mid band. Expected leverage: [−45%, −20%], central estimate ≈ −30%."

Measured: −34.4%.

Every fleet scored so far lands in its assigned band under the final dual-track diagnostic — one of them (HUST) fully pre-registered end-to-end, and one (Oxford) assigned correctly only after its original single-track call failed and forced the revision documented in §5. The sixth fleet gets its own section (§3b) with a fully public, cryptographically seeded protocol. For practitioners this is the useful takeaway: given a new fleet, early-life data alone can tell you in advance whether richer features are worth paying for.

3b. The cryptographically verifiable instance (sixth fleet, CX2)

For the sixth fleet (CALCE CX2 — a different prismatic cell and test rig from CS2), we ran the full public protocol, and this time the two heterogeneity indices disagreed — one landed in the mid band, the other near-flat. Our rule ("either-high governs") was thus facing its first hard case. Sequence, all timestamped:

  1. 2026-07-19 20:43 UTC — sealed prediction (band [−45%, −20%], falsification clause, full protocol) hashed and committed publicly: github.com/angus81226-glitch/sealed-predictions

  2. After the commit — the experiment's random seed (741333625) was drawn from the hash of Bitcoin block 958777, the first block mined after the commitment. A proof-of-work block hash is unknowable until the moment it is solved — not even the miner knows it in advance — so the results could not have existed before the commitment did.

  3. Experiment ran. Measured leverage: −21.9% — inside the sealed band. The sealed document is revealed in the same repo; anyone can re-hash it and compare against the 20:43 commitment.

One correction, disclosed in full in the repo (commitments/2026-07-20-cx2-verdict-v3-erratum.txt): the block's miner-declared header timestamp (20:33Z) predates our commit. Header stamps are not real time — in this very window, block 958776 is stamped older than its own parent — which is exactly why the protocol rests on the hash's unpredictability, not the header clock. We have since hardened the rule: future commits will name the chain tip (height + hash) explicitly, and the seed block's header time must be ≥ the commit time.

Six fleets, six correct band assignments under the final diagnostic — two of them pre-registered, one of them cryptographically verifiable by anyone. (Counting rigor: Oxford's original call failed, §5; its assignment under the revised dual-track diagnostic is correct. We count band assignments by the final diagnostic, and we count the failure openly.)

  1. Design mode: finding the best charging policy from the spec sheet

The MIT/Severson fleet cycled 124 cells under 72 distinct charging-policy strings in the authors' metadata — 64 standard two-step policies plus 8 'new-structure' variants from the follow-up batch — with measured lifetimes from 148 to 2237 cycles. We asked: can a balance-point calculation — attack energy vs. the cell's rated defense, using only public quantities (policy parameters, the manufacturer's 4A max continuous charge spec, Joule heating) — locate the optimum without lifetime data?

Results (all sealed in advance except where noted):

- The empirically best policy (3.6C to 80%) sits at balance ratio 0.978 — 2.2% from the predicted balance point of 1.0. The ratio is computed on Joule-weighted attack energy, i.e. R = (3.6/3.64)² = 0.978, not on raw current (which would give 3.6/3.64 = 0.989); the squared form follows from I²R heating and is stated here explicitly to avoid ambiguity.

- Death line: every policy above ratio 1.5 died before 1200 cycles. Correct.

- Ranking in the over-stressed region only worked after we added where-in-the-charge the stress lands (high rates late in the charge are far more damaging than the same energy early). Sealed prediction: correlation strengthens past |ρ| = 0.4. Measured: ρ = −0.60 (from −0.16). Hit.

- A second sealed refinement (rate-switch transient penalty) made things worse (ρ collapsed to −0.15). Falsified, removed, kept in the record.

4b. Full test protocols and exact parameters (reproduction-grade)

Everything below is exactly what we ran. The only items withheld are the diagnostic's selection logic; all engineering parameters are listed.

NASA Li-ion (B0005/6/18)

- EOL: discharge capacity < 80% of rated (B0005 = cycle 125)...

u/Historical_Alps_9798 — 3 days ago

Case study on the NASA C-MAPSS Turbofan Engine Degradation dataset (public, NASA Prognostics CoE): how far can data-level preprocessing alone push a completely standard model? All tests use raw files only, evaluated via last-cycle RMSE on the FD002 subset (259 engines), with RUL capped at 125.

TL;DR: three preprocessing fixes derived from a signal-vs-interference density analysis took an off-the-shelf model from 17.9 to 13.42 (-25%), matching the best published FD002 result — and the same preprocessing let a toy GRU outperform every published deep-learning result I could locate on this subset. Full recipes below.

Final results:

Baseline, off-the-shelf RandomForest, no preprocessing: 17.9

Drop the 7 zero-variance flat sensor channels + per-regime normalization + 50-cycle window: 13.7 (untuned)

Same pipeline, gradient boosting tuned on a validation split only: 13.42 ± 0.04

Reference point: the best published FD002 result I can locate is ≈13.4 (GBRT III). Its core workflow also relies on operating-regime clustering paired with normalization — the same data-level lever, found independently.

Same preprocessing, small GRU instead of trees: 16.85 on the official test set. Published deep-learning results on FD002 cluster around 18–30 (top performer ≈18.3), so our small GRU paired with data-level corrections outperforms every published deep-learning result I could locate on this subset. This proves the leverage is in the data, not in the architecture.

Why I stop here: a model-free validation. Nearest-neighbor "observation twins" — near-identical sensor states from different engines — show an RUL spread of \\\~12.6–13.0 cycles. This irreducible ambiguity originates from the simulated sensor noise and degradation stochasticity, not algorithmic limitations. At \\\~13.4, residual error is measurement-limited. The wall is in the data, not in the algorithm.

Exact recipe for test #3, so anyone can reproduce (and note it shares zero code with GBRT III — same lever, different machinery):

\\- Sensors: drop s1, s5, s6, s10, s16, s18, s19 (variance ≈ 0), keep the other 14.

\\- Regimes: k-means (k=6) on the 3 operating settings, fit on train only; z-score each channel within each regime using train statistics.

\\- Features: for each 50-cycle window, per channel take mean / std / linear slope / last value (56 dims) + 6-dim regime one-hot = 62 features. Training windows stride 2.

\\- Test protocol: last window per engine; trajectories shorter than 50 cycles padded by repeating the first row; RUL capped at 125 everywhere.

\\- Model: sklearn HistGradientBoostingRegressor(max\\\_iter=800, learning\\\_rate=0.03, min\\\_samples\\\_leaf=15, l2\\\_regularization=1.0). Config selected on a 208/52 engine validation split (6-config grid, performance variance within ±0.15). Test set touched once, 3 seeds: 13.38 / 13.44 / 13.45.

\\- Untuned reference: RandomForest(60 trees, depth 16, min\\\_samples\\\_leaf=2) = 13.69 ± 0.09.

Recipe for test #5 (GRU), full disclosure:

\\- Architecture: single-layer GRU, hidden size 24, head 24→12→1. Input = 50×14 regime-normalized sequences (same channels and normalization as above).

\\- Training: targets scaled /125; Huber loss (δ=1.0); Adam lr=1e-3; gradient clip 1.0; batch 256; training windows stride 4; \\\~10 epochs; single seed, no tuning.

\\- Evaluation: last window per engine on the official test set, identical protocol to test #3.

One critical clarification: the three core fixes were derived from a signal-vs-interference density analysis before any model was trained — computation first, verification second, no blind trial-and-error hyperparameter hunting. The only tuning performed is the documented validation-set grid search, which altered overall RMSE by roughly 0.3 cycles.

Summary: three data-level fixes took a stock tree model from 17.9 to the published-record line (25% RMSE drop), and let a toy GRU beat the entire published deep-learning field on this subset. The residual is measurement-limited. Every number is reproducible from the raw files with any standard regressor.

Why post this: the whole pipeline is transparent enough to reproduce in an afternoon, and the interesting question is no longer the model but the measurement floor. If you run it and get different numbers, post them — I am especially curious whether the observation-twin floor (\\\~12.6–13.0 cycles) holds under other feature representations.

reddit.com
u/Historical_Alps_9798 — 6 days ago
▲ 4 r/DSP

Case study on the NASA C-MAPSS Turbofan Engine Degradation dataset (public, NASA Prognostics CoE): how far can data-level preprocessing alone push a completely standard model? All tests use raw files only, evaluated via last-cycle RMSE on the FD002 subset (259 engines), with RUL capped at 125.

TL;DR: three preprocessing fixes derived from a signal-vs-interference density analysis took an off-the-shelf model from 17.9 to 13.42 (-25%), matching the best published FD002 result — and the same preprocessing let a toy GRU outperform every published deep-learning result I could locate on this subset. Full recipes below.

Final results:

Baseline, off-the-shelf RandomForest, no preprocessing: 17.9

Drop the 7 zero-variance flat sensor channels + per-regime normalization + 50-cycle window: 13.7 (untuned)

Same pipeline, gradient boosting tuned on a validation split only: 13.42 ± 0.04

Reference point: the best published FD002 result I can locate is ≈13.4 (GBRT III). Its core workflow also relies on operating-regime clustering paired with normalization — the same data-level lever, found independently.

Same preprocessing, small GRU instead of trees: 16.85 on the official test set. Published deep-learning results on FD002 cluster around 18–30 (top performer ≈18.3), so our small GRU paired with data-level corrections outperforms every published deep-learning result I could locate on this subset. This proves the leverage is in the data, not in the architecture.

Why I stop here: a model-free validation. Nearest-neighbor "observation twins" — near-identical sensor states from different engines — show an RUL spread of \~12.6–13.0 cycles. This irreducible ambiguity originates from the simulated sensor noise and degradation stochasticity, not algorithmic limitations. At \~13.4, residual error is measurement-limited. The wall is in the data, not in the algorithm.

Exact recipe for test #3, so anyone can reproduce (and note it shares zero code with GBRT III — same lever, different machinery):

\- Sensors: drop s1, s5, s6, s10, s16, s18, s19 (variance ≈ 0), keep the other 14.

\- Regimes: k-means (k=6) on the 3 operating settings, fit on train only; z-score each channel within each regime using train statistics.

\- Features: for each 50-cycle window, per channel take mean / std / linear slope / last value (56 dims) + 6-dim regime one-hot = 62 features. Training windows stride 2.

\- Test protocol: last window per engine; trajectories shorter than 50 cycles padded by repeating the first row; RUL capped at 125 everywhere.

\- Model: sklearn HistGradientBoostingRegressor(max\_iter=800, learning\_rate=0.03, min\_samples\_leaf=15, l2\_regularization=1.0). Config selected on a 208/52 engine validation split (6-config grid, performance variance within ±0.15). Test set touched once, 3 seeds: 13.38 / 13.44 / 13.45.

\- Untuned reference: RandomForest(60 trees, depth 16, min\_samples\_leaf=2) = 13.69 ± 0.09.

Recipe for test #5 (GRU), full disclosure:

\- Architecture: single-layer GRU, hidden size 24, head 24→12→1. Input = 50×14 regime-normalized sequences (same channels and normalization as above).

\- Training: targets scaled /125; Huber loss (δ=1.0); Adam lr=1e-3; gradient clip 1.0; batch 256; training windows stride 4; \~10 epochs; single seed, no tuning.

\- Evaluation: last window per engine on the official test set, identical protocol to test #3.

One critical clarification: the three core fixes were derived from a signal-vs-interference density analysis before any model was trained — computation first, verification second, no blind trial-and-error hyperparameter hunting. The only tuning performed is the documented validation-set grid search, which altered overall RMSE by roughly 0.3 cycles.

Summary: three data-level fixes took a stock tree model from 17.9 to the published-record line (25% RMSE drop), and let a toy GRU beat the entire published deep-learning field on this subset. The residual is measurement-limited. Every number is reproducible from the raw files with any standard regressor.

Why post this: the whole pipeline is transparent enough to reproduce in an afternoon, and the interesting question is no longer the model but the measurement floor. If you run it and get different numbers, post them — I am especially curious whether the observation-twin floor (\~12.6–13.0 cycles) holds under other feature representations.

reddit.com
u/Historical_Alps_9798 — 7 days ago

Case study on the NASA C-MAPSS Turbofan Engine Degradation dataset (public, NASA Prognostics CoE): how far can data-level preprocessing alone push a completely standard model? All tests use raw files only, evaluated via last-cycle RMSE on the FD002 subset (259 engines), with RUL capped at 125.

TL;DR: three preprocessing fixes derived from a signal-vs-interference density analysis took an off-the-shelf model from 17.9 to 13.42 (-25%), matching the best published FD002 result — and the same preprocessing let a toy GRU outperform every published deep-learning result I could locate on this subset. Full recipes below.

Final results:

Baseline, off-the-shelf RandomForest, no preprocessing: 17.9

Drop the 7 zero-variance flat sensor channels + per-regime normalization + 50-cycle window: 13.7 (untuned)

Same pipeline, gradient boosting tuned on a validation split only: 13.42 ± 0.04

Reference point: the best published FD002 result I can locate is ≈13.4 (GBRT III). Its core workflow also relies on operating-regime clustering paired with normalization — the same data-level lever, found independently.

Same preprocessing, small GRU instead of trees: 16.85 on the official test set. Published deep-learning results on FD002 cluster around 18–30 (top performer ≈18.3), so our small GRU paired with data-level corrections outperforms every published deep-learning result I could locate on this subset. This proves the leverage is in the data, not in the architecture.

Why I stop here: a model-free validation. Nearest-neighbor "observation twins" — near-identical sensor states from different engines — show an RUL spread of ~12.6–13.0 cycles. This irreducible ambiguity originates from the simulated sensor noise and degradation stochasticity, not algorithmic limitations. At ~13.4, residual error is measurement-limited. The wall is in the data, not in the algorithm.

Exact recipe for test #3, so anyone can reproduce (and note it shares zero code with GBRT III — same lever, different machinery):

- Sensors: drop s1, s5, s6, s10, s16, s18, s19 (variance ≈ 0), keep the other 14.

- Regimes: k-means (k=6) on the 3 operating settings, fit on train only; z-score each channel within each regime using train statistics.

- Features: for each 50-cycle window, per channel take mean / std / linear slope / last value (56 dims) + 6-dim regime one-hot = 62 features. Training windows stride 2.

- Test protocol: last window per engine; trajectories shorter than 50 cycles padded by repeating the first row; RUL capped at 125 everywhere.

- Model: sklearn HistGradientBoostingRegressor(max_iter=800, learning_rate=0.03, min_samples_leaf=15, l2_regularization=1.0). Config selected on a 208/52 engine validation split (6-config grid, performance variance within ±0.15). Test set touched once, 3 seeds: 13.38 / 13.44 / 13.45.

- Untuned reference: RandomForest(60 trees, depth 16, min_samples_leaf=2) = 13.69 ± 0.09.

Recipe for test #5 (GRU), full disclosure:

- Architecture: single-layer GRU, hidden size 24, head 24→12→1. Input = 50×14 regime-normalized sequences (same channels and normalization as above).

- Training: targets scaled /125; Huber loss (δ=1.0); Adam lr=1e-3; gradient clip 1.0; batch 256; training windows stride 4; ~10 epochs; single seed, no tuning.

- Evaluation: last window per engine on the official test set, identical protocol to test #3.

One critical clarification: the three core fixes were derived from a signal-vs-interference density analysis before any model was trained — computation first, verification second, no blind trial-and-error hyperparameter hunting. The only tuning performed is the documented validation-set grid search, which altered overall RMSE by roughly 0.3 cycles.

Summary: three data-level fixes took a stock tree model from 17.9 to the published-record line (25% RMSE drop), and let a toy GRU beat the entire published deep-learning field on this subset. The residual is measurement-limited. Every number is reproducible from the raw files with any standard regressor.

Why post this: the whole pipeline is transparent enough to reproduce in an afternoon, and the interesting question is no longer the model but the measurement floor. If you run it and get different numbers, post them — I am especially curious whether the observation-twin floor (~12.6–13.0 cycles) holds under other feature representations.

reddit.com
u/Historical_Alps_9798 — 8 days ago

Numerical Anomaly Diagnosis for Multi-Physics Coupling Simulations

I am a researcher specializing in diagnosing numerical anomalies and analyzing parameter consistency in multi-physics coupling simulations, with a self-developed mathematical framework dedicated to dissecting the mathematical root causes of simulation crashes and identifying self-consistent parameter combinations. This framework not only pinpoints problem sources but also enables reverse derivation and optimization of entire data systems. Only verified analytical conclusions will be shared—I will not disclose the internal calculation methods.

Over the past few months, I have applied this unified underlying logic to 37 cross-domain cases, covering fluid dynamics, heat transfer, structural mechanics, and electromagnetic coupling. Even when problems belong to entirely different physical domains, the framework integrates and derives insights through a single model, eliminating the need to calculate each discipline separately or align terminology across multiple experts.

My core philosophy is that all physical phenomena are composed of fundamental physical quantities; integrated mathematical analysis avoids splitting calculations by domain, streamlining the process. To clarify the scope of my research: I can perform mathematical validation of data anomaly sources, parse parameters in cross-scale coupling problems, verify the self-consistency of physical models, and optimize global parameter matching. All outputs are purely mathematical calculations—their accuracy depends entirely on the completeness and accuracy of the input data, and they are not equivalent to physical test results.

I explicitly do not handle: visual interface design, pure coding development, time-based casual consultations, or financial data analysis (my model is based on physical domains and does not apply to finance). Beyond finance, I can analyze data from all physical and engineering sciences.

If you have data or simulation problems that conventional analysis methods cannot resolve, or if you suspect logical inconsistencies in your existing computational results, feel free to discuss them with me. To improve communication efficiency, please include these details when sharing your problem: the physical field involved (e.g., fluid, thermal, structural mechanics, electromagnetics), the types of data you have (e.g., temperature curves, stress distributions, time-series data), the specific questions you want to address (e.g., why simulations diverge, whether a parameter is at a critical value, parameter tuning directions, how to reverse-optimize data), and the solutions you have already tried along with the specific bottlenecks you are encountering.

reddit.com
u/Historical_Alps_9798 — 9 days ago
▲ 1 r/ScientificComputing+1 crossposts

Numerical Anomaly Diagnosis for Multi-Physics Coupling Simulations

I am a researcher specializing in diagnosing numerical anomalies and analyzing parameter consistency in multi-physics coupling simulations, with a self-developed mathematical framework dedicated to dissecting the mathematical root causes of simulation crashes and identifying self-consistent parameter combinations. This framework not only pinpoints problem sources but also enables reverse derivation and optimization of entire data systems. Only verified analytical conclusions will be shared—I will not disclose the internal calculation methods.

Over the past few months, I have applied this unified underlying logic to 37 cross-domain cases, covering fluid dynamics, heat transfer, structural mechanics, and electromagnetic coupling. Even when problems belong to entirely different physical domains, the framework integrates and derives insights through a single model, eliminating the need to calculate each discipline separately or align terminology across multiple experts.

My core philosophy is that all physical phenomena are composed of fundamental physical quantities; integrated mathematical analysis avoids splitting calculations by domain, streamlining the process. To clarify the scope of my research: I can perform mathematical validation of data anomaly sources, parse parameters in cross-scale coupling problems, verify the self-consistency of physical models, and optimize global parameter matching. All outputs are purely mathematical calculations—their accuracy depends entirely on the completeness and accuracy of the input data, and they are not equivalent to physical test results.

I explicitly do not handle: visual interface design, pure coding development, time-based casual consultations, or financial data analysis (my model is based on physical domains and does not apply to finance). Beyond finance, I can analyze data from all physical and engineering sciences.

If you have data or simulation problems that conventional analysis methods cannot resolve, or if you suspect logical inconsistencies in your existing computational results, feel free to discuss them with me. To improve communication efficiency, please include these details when sharing your problem: the physical field involved (e.g., fluid, thermal, structural mechanics, electromagnetics), the types of data you have (e.g., temperature curves, stress distributions, time-series data), the specific questions you want to address (e.g., why simulations diverge, whether a parameter is at a critical value, parameter tuning directions, how to reverse-optimize data), and the solutions you have already tried along with the specific bottlenecks you are encountering.

reddit.com
u/Historical_Alps_9798 — 10 days ago
▲ 0 r/CFD

Skip Troublesome CFD Iterations &amp; Meshing – Analytical Flow Solution Support

I am benchmarking my proprietary analytical computational framework against real-world industrial engineering data.

If your CFD simulation fails to converge or produces unrealistic, unphysical results, I can provide precise numerical answers instantly. No meshing, repeated iteration tuning, or time-consuming software debugging required.

Information I Need From You

A short summary of your flow problem

Complete input parameters: boundary conditions (pressure, temperature, mass flow rate / velocity), core geometric dimensions, and fluid properties

Target value you want to solve (examples: critical choking mass flow, stable shockwave position, pressure drop, heat transfer coefficient)

What You’ll Get

- Precise computed numerical result

- All boundary and modeling assumptions used for the calculation

- No deep theory explanations, algorithm breakdowns, or CFD software tutorials

I’m offering the first analytical calculation complimentary. My only aim is to test and validate the accuracy of my solver using practical engineering data shared by other CFD members here.

You can share your parameters in the comment section or send me a DM, and we can solve your flow problem analytically.

reddit.com
u/Historical_Alps_9798 — 12 days ago