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APEX TECHNICAL

FDB-0025 · ORIGINAL SOURCE VALUE

MODEL-G-B7-000004

Registry: STAGEG_B7_FIRST_ENGINEERING_PREDICTIVE_VALIDATION_BASELINE_REV1__Models. Original field names and values are displayed without translation or reinterpretation.

A
MODEL-G-B7-000004
B
TESTACT-G-B4-000022
C
First-order virtual sandwich-beam response
D
Effective face flexural modulus; face thickness; total thickness; effective core thickness; core shear modulus; virtual width and span
E
D_per_width=2*Ef*tf*(h/2-tf/2)^2; compliance=L^3/(48*D*b)+L/(4*b*tc*Gc); stiffness=0.001/compliance in N/mm; delta_100=100/stiffness; P_shear=2*b*tc*tau_core
F
Face bending and core shear compliance are summed for a simply supported center-loaded virtual beam.
G
Pa|m|m|Pa
H
bending rigidity per unit width|virtual beam stiffness|deflection at 100 N|core-shear-limited load
I
N*m per m width|N/mm|mm|kN
J
LOW
K
Face thickness|effective face modulus|core shear modulus|span|bondline|fixture compliance
L
No local indentation, adhesive failure, geometric nonlinearity, edge structure, handle transition or full-paddle boundary model.
M
Analysis-only virtual coupon; not an approved laboratory method or FC002 test result. Engineering prediction for the declared Aerrow/FC002/T700/16 mm PP honeycomb/semi-hot-press working configuration under stated assumptions. The declared configuration is not proof of as-built material identity, lot identity, laminate architecture, bondline, or actual physical performance.
N
CALCULATED

Identifiers mentioned in source fields

These are search links, not inferred engineering relationships.

Provenance

archiveSha256
ded5d3a55705d2387a6fec03fd5fd9c93d948acca3c3de8c66ed7a82fca45cc5
virtual_path
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source_file_sha256
b1b1b10220f1d28fd2208ca76c5895f160a468a7cd948d219ed3494acb160483
source_locator
xlsx:sheet:5:Models:row:5
fields_sha256
32798d877ed258c9f411cb1830869d3597ce31ef3614a096f7a1800597a318de
source_version
FDB-0025