# SOL 101 — Static Analysis **Simulation:** Beam_sim1.sim **Solver:** NX Nastran SOL 101 (Linear Static) **Status:** Setup confirmed from KBS session (Gen 002). Baseline run needed. --- ## Setup — Confirmed | Item | Value | Source | Notes | |------|-------|--------|-------| | Solution type | **SOL 101** (Linear Static) | KBS session | "Solution 1 — static subcase" | | Element type | **CQUAD4** (4-node quad shell) | KBS session | ✅ Confirmed — thin shell collectors | | Property type | Thin shell | KBS session | Material inherited from "beam material" | | Mesh density | Element size = **33.7 mm** (67.4 / 2) | KBS session | Subdivision-based. Future refinement planned. | | Idealization | Promote body → mid-surface extraction | KBS session | Pair mid-surface function | ## Boundary Conditions — Confirmed | BC | Location | Type | Value | Source | |----|----------|------|-------|--------| | **Fixed constraint** | Left side of beam (full edge) | SPC (all 6 DOF) | Fixed | ✅ KBS session — "left side fixed" | | **Applied force** | Right side of beam (free end) | Point/edge force | **10,000 kgf downward** (−Y) | ✅ KBS session — "project requirement" | ### Loading Details - Force magnitude: 10,000 kgf = **98,066.5 N** (≈ 98.1 kN) - Direction: Downward (−Y in model coordinates) - Application: Right side (free end) of beam - Type: This is a **cantilever beam** with end loading — classic bending problem ## Result Extraction | Output | Method | Expression/Sensor | Status | |--------|--------|-------------------|--------| | Mass | NX expression | **`p1`** (NOT `p173`) | ✅ Confirmed — 11.33 kg baseline | | Tip displacement | ❓ Sensor or .f06 parse | TBD | Gap G3, G6 — need baseline run | | Von Mises stress | ❓ Sensor or .f06 parse | TBD | Gap G4, G6 — need baseline run | > ⚠️ **Mass expression changed:** `p1` confirmed in KBS session, replacing previous assumption of `p173`. Extractor config must be updated. ## Mesh Details | Property | Value | Notes | |----------|-------|-------| | Element type | CQUAD4 | 4-node quadrilateral, first-order | | Element size | 33.7 mm | 67.4 / 2 — Antoine says refinement is "not for now" | | Mesh method | Subdivision-based | Auto-mesh with size control | | Shell formulation | Thin shell | Mid-surface extracted from solid | | Convergence | ❓ **NOT VERIFIED** | Gap G8 partially closed (type known), but convergence check still needed | ### Mesh Estimate - Beam length 5,000 mm / 33.7 mm ≈ 148 elements along length - Perimeter of I-beam cross-section ≈ varies — but total mesh likely 10K–50K elements - Expected DOF: 60K–300K → SOL 101 solve time: seconds to low minutes ## Solver Considerations *From Technical Breakdown (Gen 001), updated with KBS data:* - **Linear assumption:** With 11.33 kg beam under 98 kN load, deflections may be significant relative to beam dimensions. L/δ ratio needs verification from baseline run. - **Mesh sensitivity:** Stress at hole edges is mesh-dependent. CQUAD4 at 33.7 mm may not fully resolve SCF at 300 mm diameter holes (~28 elements around circumference — probably adequate but needs verification). - **Mesh morphing vs remesh:** Parametric NX models typically remesh on update. Need to confirm behavior across DV range (Gap G7). - **Runtime estimate:** Single beam, CQUAD4 thin shell → likely **seconds per evaluation**. Very fast. - **Unit system:** NX model uses kg-mm-s (kgf for force). Nastran output stress in kPa → divide by 1000 for MPa. ## Validation Checklist - [ ] Baseline mass matches NX expression `p1` (11.33 kg) - [ ] Baseline displacement measured (was 22 mm at old model state — **needs re-verification** G10) - [ ] Baseline stress measured (never had a value — **G11**) - [ ] Mesh convergence verified at baseline - [ ] Mesh quality acceptable at DV range extremes - [ ] Model rebuilds cleanly at all 4 corners of design space (Gap G7) - [ ] Stress at hole edges resolved with current mesh density ## History - **Gen 001** (2026-02-09): Initial documentation from technical breakdown. All solver details pending gap resolution. - **Gen 002** (2026-02-10): Confirmed from KBS session — CQUAD4 thin shell, 33.7 mm element size, cantilever BCs (left fixed, right 10,000 kgf down), mass via `p1`. Material: AISI 1005.