Digital Research Engine · Research
DIGITAL RESEARCH LABORATORY
A unified computational environment for reproducible BLACK WIDOW research.
SHOW THE FUTURE. PROVE THE PRESENT.
DEMOLIVE COMPUTATION — COMING ONLINE
PUBLISHED REGISTRY LOADING…
RESEARCH MATRIX
| Technology | Instrument | DIGITAL MODEL | STAGE | DEMO | EVIDENCE | Live | PHYSICAL VALIDATION |
|---|---|---|---|---|---|---|---|
| C01 EPM | EPM EXPERIMENT LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C02 BW-C45 | FLIGHT DYNAMICS LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C06 GPS-Denied | NAVIGATION LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C07 Mission OS | ORCHESTRATION LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C09 Digital Twin | DIGITAL TWIN LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C10 ALBATROSS | ENERGY / TRAJECTORY LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C11 OWL | AERODYNAMIC / ACOUSTIC LAB | REFERENCE COMPARISON | — | YES | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C12 FlyScout | DEPLOYMENT / INSPECTION LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
| C13 Swarm Intelligence | SWARM LAB | DIGITAL MODEL | — | NO | AVAILABLE | COMING ONLINE | NOT PERFORMED |
RESEARCH MODULES
RESEARCH INSTRUMENT · AERODYNAMIC / ACOUSTIC LAB
QUALIFIED WITH CONDITIONSREFERENCE COMPARISONPHYSICAL VALIDATION: NOT PERFORMEDHIGHER-FIDELITY COMPUTATIONAL
Aerodynamics (Digital Aerodynamic Laboratory)
RESEARCH DIMENSIONS
airfoilCLCDCML/Dacoustic (research)
RESULT · DIGITAL MODEL
A3 / XFOIL 6.99 (viscous 2-D) + A2 (inviscid) + C11 parametric polar
- CL @ α=-4.04°
- -0.4295
- CL @ α=-2.14°
- -0.2296
- CL @ α=-0.05°
- -0.0066
- CL @ α=2.05°
- 0.2195
- CL @ α=6.09°
- 0.6564
- CL @ α=8.3°
- 0.9082
EVIDENCE
- experiment ID
- A3_TMR_CL_MATCH_01
- geometry hash
- 634c25ce132e499beb258e0d…
- campaign hash
- 9ef5349ccb9c85b1a076a575…
- reproducibility
- PASS
- package
- CONNECTED (public demo adapter)
PARAMETERS
- geometry
- DERIVED_NACA0012_TMR_dedup_v2 (DERIVED)
- reynolds
- 6000000 (DERIVED)
- mach
- 0.15 (DERIVED)
- ncrit
- 9 (SYNTHETIC)
PROVENANCE
- 01 ↓ NASA TMR NACA 0012 source (independent experimental)
- 02 ↓ TMR raw geometry (74e147db4fa052be7ab79465a756c55b39b1786bfd7141a86257e89586728ae1)
- 03 ↓ dedup-v1 (b9b001cfd039bd4307e9c31ba8e5102d5b0943832a88ea540a5741ea036f6289) [HISTORICAL]
- 04 ↓ dedup-v2 = OBJECT B (634c25ce132e499beb258e0d34684d0a18db15ee76b96fb67fc01727c95923e2)
- 05 ↓ XFOIL solver representation (35ee103cd5cfdeb807bd3a82245ccfba6f7abb489193777dc9e3d141b12e99b4)
- 06 ↓ A3Adapter -> XFOIL 6.99 -> result
- 07 ↓ comparison -> interpretation
CLAIM BOUNDARY
SUPPORTED
- — deterministic computational result
- — independent NASA reference
- — CL comparison
- — provenance-preserving evidence
CONDITIONAL
- — interpretation of the comparison
NOT ESTABLISHED
- — numerical accuracy
- — experimental agreement
- — physical validation
- — validated NACA0012
- — wind-tunnel equivalence
- — C2 closure
- — G8 readiness
- — C2: DEFERRED / WAIVED
- — G8: NOT READY
The public interface is prepared for live research execution. Current public mode uses reproducible stored (precomputed) evidence.
Deterministic computational results only. No physical validation is performed. This is a computational research environment for reproducible aerodynamic experiments.