Learnings

Not a green on 2, 4, or 6. v3 column stays empty until a third article exists.

Numbers from locked cards: PIPELINE.md, FOIL_RIG.md, ROSS_CLAMP.md, aero/cfd/stage/RUN.md, cad/stator/README.md, cad/rig/BOM.md.

Findings (v1 / v2 / v3)

# Topic v1 (foil-rig freeze, square plenum, integral catcher) v2 (gallery stator + Ø12 through-path + clamp) v3 Verdict
1 Shaft assembly Stepped stick: midspan Ø14, integral Ø16 shoulder, one-piece Ø22 catcher. 6001 ID 12 cannot pass either land. Foil ID 12.03 cannot pass Ø14/Ø22. Cannot assemble. Ø12 through-path J1→Z=97. Two-piece T1_CATCHER_CLAMP Ø22×4 after the shaft is in. 6001 then snap/collar then 7001 CE/HCP4A from the cold end. Foil IDs stay 12.03. — v1 bad. v2 good. This was a hard kill on the article.
2 Inlet feed Single pipe into a box plenum. Dump scroll r 46→66 is exhaust, not feed. One inlet loads near vanes and starves the rest. Pitch CFD assumed uniform 25/650. 360° gallery R=2.10, rounded channels, one +X boss Ø8. 4× Ø5 at 90° powder-escape (Forge signed empty-after-print). Housing OD 95, 0.228 kg. Not in the 2D pitch. — v1 bad. v2 CAD good, unproven in 3D CFD. Highest remaining aero risk on the real ring.
3 Nozzle Euler (CoolProp-on SU2) LUT/DATADRIVEN NaN at iter 2–22. Init ρ 135.147 vs table 135.919. Giles CENTRIPETAL, h0 1158 held. C 201 vs 208, α 70.7 vs 75, ρ on 22.19. Residual short of −8. Metal 19 / TE 0.35 held. — LUT bad. CoolProp+Giles good enough to move. 3% C miss is residual, not a new vane family.
4 Mixing-plane stage Not run. Frozen outer 94: Δh0 +56.5 vs Euler 40.4 (swirl-high, C_out 266), dump P 14.02 vs 13.89, nozzle C 181 vs 208, α 69.4 vs 75, rotor C 266 vs 120. Older 200-iter card was C 201 / +51. Continue flipped Work −7 (rotor adding h0) — killed. rms −2.17/−2.03 vs −8. 61 is the old mis-labeled static, not the freeze comparator. — +56.5 vs Euler-40 is swirl-high. Rotor C_out is bad. Do not iterate that restart. Viscous still NaN. Not a green on 6.
5 Wheel / mean-line 48.00 / 13 / finish TE 0.40, PR 1.8, Δh0 75.9, η_tt 0.802. Disk cent ur 0.0148 vs Stage 0.019. Soak 0.20. Unchanged. Axial and jet-stack families already rejected. — Good. Do not reopen the machine class.
6 Catcher / ROSS One-piece 282 Ø22×4 on 0.148 kg stick. Paper first pair 25.5k. Print 0.123 + 17-4 clamp 0.008 = 0.131 kg; + T1_7001_IR 0.0063 kg (named B3DO inner ring, not balls+outer) at Z=92.0. First pair RT 25.2k at k=1e6 / 54.7k at 5e6. 24.1k / 52.4k (+0.019 complete-bearing cap) is history. No-7001 pair on this mesh is history. 20k under on paper. UNSIGNED. 17-4 H1025 is done above ~300 C — 20k cold only. 650 C column is 282-beam paper, not a clamp cert. Do not invent inner+balls rpm. — 20k cold paper is consistent. Hot clamp is bad. Residual cert still required. Do not green 2.
7 Case 17-4 bar, CASE_OD 70, hot flange 96, ~19 mm wall over Ø32 foil bore, 2.948 kg. Lab block, not hoop-min (25 MPa membrane on r=36 wants a few mm of 282). Same alloy. Pocket Ø28 for clamp lugs, 2.914 kg. Not thinned. One-piece. — Fine for a lab housing. Bad if you wanted a light can. Do not thin for the 20k article.
8 Quote / AM Velo pack Z=72 / print TE 0.55, stub volute, no catcher. HIP 1175/150/4 h + 1135 + 1010+788. No AFM on TEs. Quote hashes frozen. Ø12 land is post-HIP machine, not a Velo resend. Clamp is 17-4 bar, not 282 print. Gallery 4ר5 HIP-emptyable. — Quote freeze is good. Do not mix clamp into the 282 heat.
9 Coupon / Sy — Blank Ø12×85 Z ×6 + 2 flats. Not a 650 C AM Sy. 550/650 mass gain missing. — Blank is good. Cert is missing. Do not green 4.
10 CFD process Ideal-gas / LUT as the sign. In-process CoolProp HEOS. Giles n/t/s, not Cartesian. Mixing-plane inner 1 was cold; 20 inner took. Blind continue flipped the stage. — CoolProp-on is good. Blind restarts are bad. Freeze fields that hold Δh0.
11 Foil journals Cans Ø32, film 0.015, ID would not pass v1 steps. Foil IDs 12.03 locked. Shaft Ø12 through the cans. Eddy at Z=66 still sees Ø12. k 1e6–5e6, 20k under first pair 25.2k (T1_7001_IR 0.0063). — v2 good. Do not grow IDs. Do not treat foil k as 5e7.
12 Axial locate / thrust SKF 51101 20–40 N. Catalog 9k / 13k — 20k is not a spin plan on that part. 7001 CE/HCP4A 12×28×8, grease attainable 98k, preload 17–40 N. Pocket Ø28. Still not 25 MPa. — 51101 at 20k is bad. 7001 is the catalog-legal locate. Do not green a hot machine on either.
13 Trip Written ID ≥400 C. Not wired. 0.20 not trip-safe. Same. Type N Ø1.5 (ID A/B, RIM, GAS) on paper only. Cold 20k does not wait. — Law is good. Hardware is missing. Do not grow the 0.20 to “fix” trip.
14 AMB / 80k Parked. Bare Ø12 cannot make ≳5e7 (pole area). Still parked until a 20k dwell exists. Sleeve target: pole ~22, gap 0.15, ≳5e7. — Park is good. Electrify after the spin, not instead of it.

EE freeze (Magneto, 2026-08-31)

P0-1 / P0-2 / P0-3 stay accepted review findings — do not delete, do not soften. P0-3 stays the 51101 catalog finding; the 7001 pick is the live locate (already the note under P0-3). No more EE geometry on this article.

Redesign, ranked by probability of actual impact

What we would change on a complete next article (v3), not a doodle. Probability is of moving a locked number (assemble, C, Δh0, first pair, hot soak) — not of looking nicer.

Rank Change Why Impact Apply when
1 Keep Ø12 through-path + split catcher (do not revert v1 shaft) v1 could not be built. Everything else is fiction until the stick goes through the cans. Certain Already v2. Never go back.
2 3D inlet gallery in the CFD (or a 360° inlet BC that is not a 2D pitch) v2 CAD feeds all 19 vanes. The pitch still assumes uniform 25/650. Maldistribution is the failure mode Kevin called on day one. High Before signing ṁ or vane TE on the real ring.
3 Mixing-plane / rotor work (solver first, metal second) Frozen Δh0 +56.5 vs Euler 40.4 is swirl-high (C_out 266) on a field that is not converged. Rotor C_out 266 vs 120 is not. Continue already flipped the sign of Work. 61 is the old mis-labeled static, not the freeze comparator. High (on Δh0/C_out) Next CFD. Recut 13 / 0.40 / Ø48 only if a clean residual still dumps C_out ≫ 120.
4 Hot catcher in 282 (or drop the runner for a hot soak) 17-4 clamp is 20k cold. H1025 is finished above ~300 C. A 650 C article cannot use this runner. High for a hot machine, zero for the 20k cold spin Only if the next article soaks 650 C.
5 Viscous ECM wall (ks signed, not 5 μm label) Euler nozzle is 201/208. SST NaN'd at iter 0. η_tt 0.802 cannot be signed inviscid. Medium-high for green 6 After a mixing-plane field that does not flip.
6 Case as a real 25 MPa vessel, not a Ø70 bar block Wall is locational stock. Fine for 20k. Wrong mass/OD if this becomes a packaged stage. Medium for a product, low for T1 v3 package, not the foil rig.
7 Parametric vane β / throat (N=19, metal 73°, α2=75°) Nozzle Euler already 3% on C. Mixing-plane C 181 is the dirty field, not a proven throat miss. Low-medium Only after rank 3 plateaus with residual < −8.
8 Micro-feed nests around the ring Printable but Forge will not sign a nest we cannot empty. 4ר5 gallery already has a gas path. Low Do not.
9 Sleeved AMB (pole ~22, 0.15 gap, ≳5e7) Foil 1e6–5e6 crosses before 80k. Bare Ø12 AMB sits on ~1e7. Sleeve is the 1.8× split. High for 80k, zero for the 20k cold spin After a residual cert + 20k dwell. Not this article.
10 Real 25 MPa thrust (not 51101) 51101 is 20–40 N locate. Radial k does not hold 25 MPa. Catcher clamp is a runner. High for a pressurized hot machine, zero for the cold foil spin Second CAD, with the sleeved AMB.

v3 is not opened. Rank 1–2 are CAD we already have. Rank 3 is Stage. Rank 4 is Forge if we ever go hot. Rank 9–10 are Magneto after 2 is a run. Do not recut vanes or the quote pack on this list.

CAD lock

Existing stills only — tables stay the authority. Assembly: foils in case, shaft from the hot end, clamp, 6001, snap/collar, 7001, cover.

v2 shaft through-path and two-piece catcher clamp
Ø12 through-path J1→Z=97 — two-piece T1_CATCHER_CLAMP Ø22×4 after the shaft is in (not thru), foil IDs 12.03, 1 mm air to clamp, no Ø14 swell, no integral Ø16. Findings 1 + 11.
v2 360 degree inlet gallery
360° inlet gallery R=2.10 — 19 vanes, ID 48.40, TE 0.35, 4× Ø5.00 at 90° powder-escape. Not the dump scroll. Not cad/rig. Finding 2.
v2 T1-CASE Ø28 clamp pocket
T1-CASE 17-4 — CASE_OD 70 / FLANGE_HOT_OD 96, Ø28 clamp pocket, Ø28.30 6001, 2.914 kg. Not thinned, not 25 MPa hoop-min, not a generator can. 51101 pocket is locate, not 25 MPa. Finding 7.

Blank slate (if T1 did not exist)

This is not a v2 delta. It is what Hardwar would build instead of a 48 mm / 80k / foil / 282-stick that also wants 25 MPa / 650 C.

The core mistake was one article doing three jobs: a 20k foil spin, an 80k rotordynamic target, and a 25 MPa / 650 C aero stage. Those want different shafts, different bearings, and different materials. v1/v2 keep gluing them.

If starting over What, specifically Why this beats T1
Two machines, not one (A) Cold spin rig: steel/IN718 shaft, dummy or bolted wheel, split 17-4 housing, balls or foils to 20–40k. (B) Hot aero article: 282 wheel+nozzle only, no foil cans, no 17-4 clamp, real thrust TBD. Catcher-in-the-print, 17-4 at 650 C, and 51101-as-thrust are all symptoms of the glue.
Split housing from day one Horizontal split or a two-flange case (hot gas can + cold bearing cartridge). Never a one-piece through-bore with foil IDs of 12.03 and features on both sides. v1 was unassemblable. v2 through-path works; a split case is how every turbocharger avoids that class of bug.
Wheel shrunk or bolted on a machined shaft Print the 48 mm / 13-blade wheel as a disk, HIP, ECM TEs, then shrink/bolt onto a ground Ø12 steel or 718 shaft. Catcher / 6001 / 51101 live on the shaft, not in the 282 print. We HIP'd a stick we then turned to Ø12. Quote Z=72 already admitted the print should end at the wheel.
Same U, bigger / slower Keep U2 ≈ 201 m/s. 80 mm tip @ ~40k instead of 48 mm @ 80k. Same Wright-class work. Foils, catcher, and residual all get easier. Print is still 282. 80k foil + G2.5 at 0.044 g·mm is the hard shop problem. We have not even spun 20k.
Or commit to 80k bearings first If 48 mm / 80k is non-negotiable: size foils for 80k (or sleeved AMB) on day one. Do not learn 20k catcher-only and call U=201 a later-stage label. T1's 20k article does not validate the mean-line speed.
Inlet scroll first, dump second Design the 360° feed (or a real inlet volute) before the vane ring. Dump collector is easy. Starved vanes are not. 3D CFD of that gallery before a 2D pitch. v1 dumped a box plenum. v2 CAD has the gallery; CFD still assumes uniform pitch.
Keep single-stage radial PR 1.8 Do not go axial. Do not go a jet stack. Do not go 200 kW. Sandia/Wright class is the right machine. Already rejected. Blank slate does not reopen it.
Gas-path 282 only Shaft and catcher not in the 282 heat. Clamp/hot runner in 282 only if the article is actually hot. Case stays 17-4 or 316 for cold; a 25 MPa can is a different part. Mixing 282 stick + 17-4 clamp + 650 C paper is how we got a clamp that cannot soak.
Thrust as a named problem Balance piston / dummy piston / real gas thrust. Never 51101 20–40 N with a catcher disk labeled “not thrust.” 25 MPa × eye area is orders above 40 N.
Type N in the first cut Bosses and Ø1.5 holes in the first case, wired before the first dwell. Traveler exists. Cold 20k does not wait, but the bosses should have been in v1 as-built.

What I would not change: 282 HIP+HT, ECM/remelt TEs (no AFM), soak 0.20, odd blade count, CoolProp HEOS, no γ, catcher-only as a *backup* not a bearing.

Hardwar pick if Kevin wants a v3 blank slate: split the program. Cold split-case spin rig on a machined shaft (this year). Hot 282 stage as a second CAD, inlet gallery in the CFD, real thrust, no 17-4 in the gas. Keep 48/80k only if Magneto is on 80k bearings now; otherwise grow the wheel and drop rpm.

Stage (aero / ROSS)

U2 = 201 m/s at 80k, r = 24 mm. Spouting C0 = √(2 Δh_is) ≈ √(2×75.9e3) ≈ 390 m/s. U/C0 ≈ 0.52, not U/C2 = 201/208. Dixon radial-inflow peaks near U/C0 ≈ 0.70. We are a low-work PR 1.8 stage running slow on that chart, or a 48 mm wheel asked to do 80k foil work it cannot dump in 2D.

What is good vs bad (Stage lane)

Good Bad
CoolProp HEOS + Giles n/t/s + AREA h0 held 1158. MIXEDOUT flashes solid. Cartesian Giles never made 75°. Residual never −8.
Nozzle Euler 19 / TE 0.35 C 201 vs 208 (3%). Architecture held. α 70.7 vs 75. Not a new vane.
Mixing-plane freeze outer 94 Δh0 +56.5 vs Euler 40.4 (swirl-high, C_out 266). Dump P 14.02 vs 13.89. last_good/ on disk. 61 is the old mis-labeled static, not the freeze comparator. Nozzle C 181 vs 208. Rotor C 266 vs 120. rms −2.17/−2.03.
Blind continue — Work −7. Rotor adding h0. Do not iterate a +Δh0 field.
Viscous SST/SA — NaN / C~30. SU2 8.5 wall function will not take ks=5 μm. η_tt 0.802 is unlabeled Euler.
2D midspan H-mesh Cheap, CENTRIPETAL saw ~19 / ~14 blades. No exducer (Japikse rotor exit is axial). Mesh dumps at r≈10 mm, wrap 42°. That is why C_out stays ~2×. No tip gap. No gallery.
ROSS clamp-on 20k under RT 25.2k / 54.7k at foil 1e6–5e6 with T1_7001_IR 0.0063. Print 0.123 + clamp 0.008 + IR 0.0063. UNSIGNED. Zero-speed, no gyro, not a Campbell. 650 C is 282-beam paper. 17-4 clamp is 20k cold.
0.20 tip Mean-line label. Not trip-safe vs thermal. Do not grow it to “fix” trip.

Blank slate, ranked by actual aero/ROSS impact

If T1 did not exist. Probability is of moving C_out, Δh0, U/C0, or first-pair — not of a prettier pitch.

Rank What I would do instead Why it beats this article When
1 Two machines. Cold 20k spin on a ground shaft. Hot 25 MPa / 650 C stage as a second CAD with real thrust. 20k foil + 80k U=201 + 25 MPa on Ø12 is why C_out, clamp soak, and 51101 are all lying. Mean-line 80k is not validated by a 20k dwell. Program split. This article stays the cold one.
2 3D radial-to-axial rotor + 360° gallery CFD before any 2D pitch. Exducer is axial (Japikse). Inlet gallery is the ring, not a Riemann 25/650. Frozen C_out 266 vs 120 is a 2D dump at r=10, not a 13-blade proof. Gallery maldistribution is still unsigned. Next CFD on this article (Hardwar rank 2–3). No recut until that residual is clean.
3 Size U/C0 toward 0.7 (Dixon) or admit PR 1.8 is a low-work wheel. Keep U2=201: ~80 mm tip @ ~48k, not 48 mm @ 80k. Same Wright PR 1.8. 0.52 is off the usual radial peak. Growing D at fixed U drops rpm into the foil band. 48/80k is the hard shop problem we have not spun. v3 only. Do not grow this 48 mm print.
4 Mixing-plane freeze rule. Copy last_good when Δh0 > 40 and C_nozzle > 180. Never continue that field. Relative-frame dump, not more OUTER. Continue already reversed Work. More iters is not a design change. Now. Already frozen +56.5.
5 Campbell with gyro before anyone says 80k. Undamped k-sweep is a 20k paper gate. FW/BW split at 80k is a different number. 25.2k first pair does not protect 80k. After a 20k dwell, with Magneto k.
6 Viscous ECM wall after the Euler freeze, ks signed by Forge. η_tt 0.802 stays unlabeled until a residual exists. SST NaN’d. Wall function vs roughness is a solver limit, not a TE recut. After rank 4 holds.
7 Cold tip larger, or matched stator soak — not 0.20 as trip. 0.20 vs thermal was already a kill for trip-safe. Growing 0.20 is not a redesign. Hot article only.

What I would not change: single-stage radial PR 1.8 (Sandia), odd blade count, CoolProp HEOS (no γ), 13 / 0.40 / Ø48 on this article, ECM/remelt TEs, soak 0.20 as a cold label, catcher as backup not a bearing.

Stage pick if Kevin wants a blank slate: same split as Hardwar. Aero article is 3D gallery + R-A exducer, U/C0 sized on Dixon, CoolProp mixing-plane frozen at +Δh0. This foil rig stays 20k cold on the Ø12 stick. Mixing-plane residual is still first here. Do not recut 13 / 0.40 / Ø48 on the learnings list.

360° gallery / full-annulus feed (Stage paper card, item 6 step (6))

Locked CAD (cad/stator/README.md): gallery circular R=2.10 mm, 360° annulus; one +X boss Ø8; powder escape 4 × Ø5 at 90°, empty-after-print — stay open on 20k cold, 25 MPa article plugs. Feed, not the dump. Quote hashes stay. Not a recut of cad/rig. Not a Velo send.

Area (geometry, not flow) Formula mm²
Gallery passage π R², R = 2.10 ≈ 13.85
4 × Ø5 open 4 × π (2.5)² ≈ 78.5

4 × Ø5 open is ~5.7× the gallery passage. Empty-after-print, not a pressure wall — left open at 25 MPa they dump the ring. 20k cold: leave them open. 25 MPa article: plug. Do not treat open Ø5 as a sealed feed.

Why a 2D pitch + uniform Riemann 25/650 cannot close ring feed: one periodic pitch with a uniform Riemann 25 MPa / 650 C inlet assumes every vane already sees the same total. The day-one starve is the opposite: one +X boss into a 360° R=2.10 gallery — near vanes loaded, far vanes starved — and a 2D pitch cannot see that azimuth. Periodic 2π/19 plus a uniform total is the assumption, not the proof. 2D pitch mass is not ring ṁ: MEANLINE.md — ṁ is unsigned until a 3D gallery exists.

A later full-annulus run must report: ṁ split across the 19 throats (near-boss vs far); Pt loss from the +X boss to each throat; α spread at the 19 throats vs 75°. Until those three exist, chip 6 stays OPEN. Not this freeze. Not a mixing-plane continue. Full card: aero/cfd/GALLERY.md.

Fine 3D exists (NPOIN 61352) — unsigned, not conserved. Do not continue OUTER. Chip 6 still OPEN. Card: aero/cfd/gallery/RUN.md.

Forge (AM / metals)

What is good vs bad (Forge lane)

Good Bad
Alloy in clean sCO2 Chromia former. 750 C / 20 MPa / 1000 h: AM 282 0.60–0.61 vs wrought 0.48 mg/cm². Scale ~2 µm Cr2O3, internal ox ≤20 µm (Magnin). 740H 0.25–0.29 is thinner scale, not a reason to dump 282 creep. 550/650 C AM mass gain is MISSING. 750 C RG is not a 650 C carburization cert. Pint: O2/H2O impurities move gain more than AM vs wrought.
HIP+HT recipe Velo: HIP 1175 C / 4 h / rapid cool → vac 1135 / 30 min → 1010/2 h + 788–790/8 h. Two-step age (Joseph GB carbides). Do not furnace-cool HIP. Do not ASME 802 C single-step on a rotor. 150 MPa is Deshpande fill (1185/150/3.5 h), not Velo-published. Silent P on a PO is a process miss.
TE finish Print 0.55 / finish 0.40. No AFM on TEs — unconstrained AFM TE removal 0.29 mm. ECM or remelt only. ks = 5 µm is UNSIGNED. As-built Sapphire Ra is not an ECM wall. Viscous CFD cannot take a label.
Powder escape 4 × Ø5.00 at 90°, empty-after-print. First ports were too small to HIP-empty a 360° gallery. Do not nest micro-feeds we cannot empty.
Quote pack Z=72 / 0.55, no catcher, two 282 prints (wheel + ring). Catcher off the heat is the right split. We still HIP a shaft (Z=0–72) then turn the span to Ø12. Paying AM + HIP distortion for a grind journal.
Disk / Sy Wrought sheet Sy 631 MPa at 649 C vs rim VM 246 (margin on the sheet). AM Sy after OUR HIP+HT is unsigned. EOS 658 MPa horiz @650 C is 1250 C Option-1, not 1175/150/4 h. Coupon Ø12×85 is a blank, not a cert. Sequence was quote-the-wheel first.
Clamp / 17-4 17-4 H1025 is fine as a 20k cold runner. H1025 is done above ~300 C. Ø12 282 conducts from a 650 C disk — “cold end” Z=72 is not a thermal break. 17-4 cannot live on a hot article.
IN718 backup Label only. Not drop-in. Worse 650 C creep rupture, different HIP/HT. Do not quote it as primary.

Powder-port state (4ר5): empty-after-print stays. On the 20k cold rig they stay OPEN — not a pressure wall. On a hot 25 MPa article they are plugged after HIP — 4×π×2.5² ≈ 78.5 mm² cannot sit in a 25 MPa boundary. Do not recut the gallery 4ר5. Do not nest micro-feeds.

Blank slate, ranked by actual metals impact

If T1 did not exist. Probability is of moving AM Sy, HIP distortion, hot-soak alloy, or a signed ks — not of a prettier print.

Rank What I would do instead Why it beats this article When
1 Coupon first. E21 Ø6.0×30 / GL 24 at 650 C after the exact traveler (HIP 1175/150/4 h + 1135/30 + 1010+788). Set C: 650 C / 20 MPa sCO2, 500–1000 h, mass gain. Then quote the wheel. FEA is on wrought 631. AM Sy is the disk gate. 750 C RG does not close 4. We reversed the sequence. Before any Velo PO. Closes 4.
2 Print gas-path 282 only. Wheel as a short disk (HIP-stable Z), nozzle ring with empty-after-print ports. Shrink or Hirth onto a ground 718/steel shaft. Journals are ground, not AM lands. Catcher/6001 live on the shaft. HIP 1175/150/4 h on a slender stick warps. We then machine the whole span to Ø12. Quote Z=72 already admitted the print should end at the wheel. v3 architecture. This article stays the Ø12 stick.
3 Two alloy articles. (A) 20k cold: 17-4 case, steel shaft, 17-4 clamp. (B) 650 C / 25 MPa: 282 wheel+nozzle only. Any runner that can see >300 C is 282 or 718, never H1025. 17-4 clamp + 650 C paper on one stick is how we got a runner that cannot soak. Conduction along Ø12 282 will heat Z=72. Program split. Same as Hardwar rank-1, with the °C cut.
4 Sign ks from a PECM/remelt coupon Ra, not a 5 µm label. AFM stays off 0.40 TE (0.29 mm kill). PECM vs laser remelt is the TE fork (Gradl/MSFC PECM analog, recast vs electrolytic). Stage viscous NaN’d on an unsigned wall. η_tt 0.802 is unlabeled Euler until ks is a measurement. After mixing-plane freeze. Closes the wall, not the vane.
5 Put HIP P on the PO. 150 MPa Ar as a stated Deshpande substitute, or get Velo’s number. Rapid cool, no furnace cool. Keep 1135/30 — do not skip. Keep two-step age. Silent 150 MPa is how a traveler drifts to 100 MPa / 1250 C (Shaikh/EOS) and we lose the grain-size/creep card. Same PO as rank 1.
6 Do not swap 282 for 625/740H on RG, and do not open IN718 without a separate 650 C rupture card. Thinner scale at 750 C is not higher rim Sy. 282 is the γ' creep pick. Never on this class.

What I would not change: Haynes 282 on the gas path, two-step 1010+788, no AFM on TEs, print-fat 0.55 / finish 0.40, 4ר5 empty-after-print, quote cut before the catcher, coupon as a traveler (but run it first).

Forge pick if Kevin wants a blank slate: same split as Hardwar. Coupon + HIP-P on the PO before metal. Print a 282 disk, not a 282 stick. 17-4 never in the 650 C conduction path. This foil rig stays 20k cold. Do not recut 13 / 0.40 / Ø48. Do not green 4.

External review (31 Aug 2026) — what we take

Accepted (P0)

# Finding Evidence on our disk Action
P0-1 Case and cover occupy the same metal. Review: ~29 065 mm³ common (~75% of cover). T1-CASE cold flange is Z=100–108, Ø80. T1-COVER is Z=99.2–108, Ø80. The cover was modeled on top of a flange the case already owns. @B3DO new assembly rev: case ends at the mate (Z=100), cover is the plate + spring boss only. Recalc spring working length. Do not thin the case.
P0-2 Euler work ≠ displayed Δh0 75.9. With U2=201, C2=208, α2=75°: Cθ2=201 m/s. Zero-exit-swirl work U2 Cθ2 ≈ 40.4 kJ/kg. Cap at |C3|=120 is ~49 kJ/kg, not 75.9. Static drop 1136−1075=61 was labeled Δh0. MEANLINE.md table vs _eta.json 75.9. Review identity is correct. CoolProp cannot fix angular momentum. @Stage closed aero/MEANLINE.md at 40.42; CFD target 40.4. Frozen mixing-plane +56.5 vs Euler 40.4 is swirl-high (C_out 266), not a miss of 75.9 and not a miss of 61. 61 is the old mis-labeled static drop. Do not retune vanes to 75.9.
P0-3 SKF 51101 catalog speed is below the 20k dwell. Review: SKF reference 9 000 / limiting 13 000 rpm. Preload 20–40 N does not raise that. We named SKF 51101, Z=88–97, 20k ceiling. @Magneto pick a thrust part whose catalog envelope covers the dwell, or drop the dwell below the catalog limit. 20k on 51101 is not a spin plan.

Magneto’s pick is SKF 7001 CE/HCP4A (finding 12 / /ee). P0-3 stays the accepted review finding — 51101 catalog is below 20k.

Accepted (P1, do not green)

Finding Take
Shaft is hollow Ø12 / Ø10. Snap groove Ø11.50 leaves 0.75 mm wall. Solid-Ø12 I is ~1.93× this tube. “Ø12 through-path” hid the bore. @Stage ROSS/FEA must use the tube + groove + clamp + collar + snap + rotating washers, not a solid 0.123 kg stick. Until that hash matches CAD, 25.5k stays paper.
Two rotor solids in one STEP (print + finish) BOM/inertia/collision must have one active rotor. Print-vs-finish is a compare config. @B3DO.
Mixing-plane outer 94 is a checkpoint, not a solution Already frozen. Residual ~−2. Do not call it last-good as if converged.
Nominal 0.20 gap ≠ running clearance Soak label only. Budget orbit + cent + thermal + foil 15 µm + catcher 150 µm at their own stations. Do not grow 0.20 to “fix” trip.
V2 gallery R=2.10 is a size, not a proof of uniform feed 2D pitch cannot sign the ring. Powder ports need an operational state (plugged vs flow).
Coupon blanks are bars, not thin-feature witnesses Keep blank ≠ Sy. Next coupon set needs TE/wall witnesses. 4 stays open.

Not taken as a recut

Next steps (this article, in order)

Step Owner Question Done when
1 B3DO Can the parts coexist? Case/cover no volume interference (split Z=100 mate). One active rotor in the rig STEP. Spring working height declared. Sequence: foils → shaft → clamp → 6001 → snap → 7001 → cover.
2 Stage Does the duty match the triangles? Closed in aero/MEANLINE.md. Euler Δh0 = 40.42 kJ/kg (U2=Cθ2, Cθ3=0, r3=9 mm). 75.9 was η_ts×101 totals; 61 was static h2−h3 mis-labeled Δh0. CFD export is 40.4, not 75.9. ṁ still unsigned.
3 Magneto Can the cold rig run at its ceiling? 51101 is out (catalog 9k/13k). Locate is SKF 7001 CE/HCP4A 12×28×8, pocket Ø28, grease 98k, preload 17–40 N. Still not 25 MPa. 2 stays open until a residual cert.
4 Stage Does ROSS/FEA describe this shaft? Tube Ø12/Ø10, groove, clamp 0.008, collar, snap. 7001 rotating mass is named T1_7001_IR 0.0063 kg (inner ring only, not balls+outer). First pair 25.2k / 54.7k unsigned. Catalog 0.019 / 24.1k is comparison only. Do not invent inner+balls rpm. Still no gyro. Hash vs STEP. Chip 2 stays OPEN.
5 Stage Is CFD a solver bug or a design miss? Card, not a green. File aero/cfd/SOLVER_VS_DESIGN.md. Freeze +56.5 vs Euler 40.4, not vs 61, not vs 75.9. Extra is 2D exit swirl (C_out 266). Keep last_good. No continue into −7. 19 vs 13 pitch scaling. Chip 6 OPEN. SST NaN at iter 0 is a solver card, not a TE recut.
6 Stage Does the gallery feed 19 vanes? Full-annulus or a 360° inlet BC. 2D pitch cannot close this. Paper card aero/cfd/GALLERY.md: bore ≈13.85 mm² vs 4ר5 ≈78.5 mm² — areas, not a ring ṁ. Chip 6 stays OPEN.
7 Hardwar / Stage Does any transient eat the 0.20? Clearance budget vs time. Not a trip-safe claim.
8 Forge Thin-feature process Set D — TE / wall witnesses on a later plate (COUPON.md Set D), not a recut of the frozen Ø12×85 bars+flats coupon STEP. Rotor TE 0.55→0.40, stator TE 0.55→0.35, ECM or remelt, no AFM. Ra→ks — 5 µm stays UNSIGNED until that number. 4 stays OPEN until set A 650 C Sy (E21). Set D does not green 4. ks does not green 6. No PO.
9 Stage Aero DOE Only after steps 2 and 5. No 13-count change to force 0.802.
10 Hardwar Cold hardware Only after 1, 3, 4. Residual cert + catalog-legal dwell. Still no PO from this list.

Review 31 Aug (Stage takeaways)

P0 work identity is real. Closed: Δh0 = 40.42 kJ/kg (aero/MEANLINE.md). Do not tune mixing-plane to 75.9. Frozen +56.5 vs Euler 40.4 is swirl-high; C_out 266 is swirl, not a 13-blade kill and not a 61 miss. 61 is the old mis-labeled static drop, not the freeze comparator. Chip 6 stays OPEN.

P1 hollow shaft: clamp ROSS already uses Ø12/Ø10 (BORE_M=0.010, snap Ø11.50). Not a solid beam. Current first pair RT 25.2k / 54.7k is T1_7001_IR 0.0063 kg (inner ring only). Catalog 0.019 / 24.1k is comparison only. Still not a Campbell: no gyro, no residual cert. Chip 2 stays OPEN. UNSIGNED.

Snap groove 0.75 mm wall on Ø12/Ø10: fine as a 20k cold machine land. Not an 80k 282 notch card. Not a recut.

P1 “last good” is a freeze, not a converged solution. Chip 6 stays OPEN.

Do not recut 13 / 0.40 / Ø48 on this review.

v3 stays closed. Quote and gallery hashes stay unless step 1 forces a case/cover rev.