BLACK WIDOWResearch Program
#06Simulation OnlyDIGITAL EVIDENCE ONLY

OWL

Leading/Trailing Edge Serration Research

Research Question

Do owl-inspired leading/trailing edge serrations produce statistically significant improvements in lift-to-drag ratio (dL/D >= 5%) or sound pressure level (dSPL >= 5 dB)?

Digital Model

Type

Parametric Aerodynamic Sweep

Version

v1.0.0

Plugin

c11_owl

Core Variables

21-point alpha sweep, CL, CD, L/D ratio, airfoil geometry, serration parameters

Main Assumptions

Parametric CL/CD model; xfoil_validated = false; no wind tunnel data; no CFD validation; no acoustic measurement

Model Boundary

2D parametric polar only; no 3D effects; no Reynolds number variation; no surface roughness; no flutter analysis

Inputs / Parameters

ParameterValueUnitProvenance
Alpha range0-20degDESIGNED
AirfoilNACA 4412 + serrations—DESIGNED
Serration geometryowl-inspired—ASSUMED

MEASURED = 0 parameters across all 9 technologies. Physical calibration deferred.

Experiment

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What This Result Does Not Prove

This result does NOT prove: actual aerodynamic improvement, serration effectiveness, acoustic reduction, or structural safety. xfoil_validated = false. PARAMETRIC AERODYNAMIC MODEL ≠ EXPERIMENTALLY VALIDATED AERODYNAMICS.

Next Research Step

NEXT DIGITAL STEP

Execute sim-xfoil-owl (E-010 M1). Run sim-openfoam-owl. Flutter FEA + tap test.

FUTURE PHYSICAL / CALIBRATION STEP

Complete E-011 prototype. Wind tunnel testing. Acoustic testing. Deferred.

Role

OWL researches owl-inspired leading/trailing edge serrations for passive aerodynamic (dL/D) and acoustic (dSPL) benefits. Campaign C04.

Digital Results

C11 OWL parametric aero sweep executed. L/D curve generated with parametric model. Simulation-only.

Physical Results

No wind tunnel tests. No acoustic tests. OWL insert STLs in inventory (79-part set). Partial LE photos from audit. No flutter tap test.

Proven

C11 parametric aero sweep: L/D curve generated. OWL LE/TE configurations specified in PDR. Insert STLs listed. Falsifiable hypothesis with null-publish rule.

Not Yet Validated

dL/D >= 5% (XFOIL NOT RUN). dSPL >= 5 dB (acoustic tests NOT RUN). Flutter risk unknown for TE serrations. All results parametric/simulation-only — no XFOIL/OpenFOAM validation.

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