No document is open. Use File > New, or open one of the examples, first.
*Name
Part Number
Parent
Sequence
Step
Layup Surface
Net Boundary
Extended Boundary
No records in this document yet. Right-click, or use Create New, to add one.
Start a laminateNothing is open. Choose one of these.
Published components
Reproducing a published stacking sequence means the transcription is right and the laminate is internally consistent. It is NOT a strength, buckling, producibility, drape, airworthiness or qualification claim, and none of these documents is a flight article. Each number carries whether the source PUBLISHED it, we CHOSE it, or it is DERIVED from the two.
NTRS 20140011912Cylindrical panel · radius 203.2 mm · 319.2 mm arc × 406.4 mm axial · 8 plies · 1.016 mm nominal · [-45/+45/0_2]s-45°0°45°Shell nominal radius 8.0 in / 203.2 mmPUBLISHEDShell nominal length (axial) 16.0 in / 406.4 mmPUBLISHEDSector angle 90deg (1/4 of the shell)CHOSENSector arc length (tool u extent) 319.186 mmDERIVED
NTRS 20140011912Cylindrical panel · radius 203.2 mm · 319.2 mm arc × 406.4 mm axial · 8 plies · 1.016 mm nominal · [-45/+45/90_2]s-45°45°90°Shell nominal radius 8.0 in / 203.2 mmPUBLISHEDShell nominal length (axial) 16.0 in / 406.4 mmPUBLISHEDSector angle 90deg (1/4 of the shell)CHOSENSector arc length (tool u extent) 319.186 mmDERIVED
NTRS 20140011912Cylindrical panel · radius 203.2 mm · 319.2 mm arc × 406.4 mm axial · 8 plies · 1.016 mm nominal · [-45/+45/0/90]s-45°0°45°90°Shell nominal radius 8.0 in / 203.2 mmPUBLISHEDShell nominal length (axial) 16.0 in / 406.4 mmPUBLISHEDSector angle 90deg (1/4 of the shell)CHOSENSector arc length (tool u extent) 319.186 mmDERIVED
NASA/TM-20205008667The project opens, but curved laminate buildup is currently refused at the internal ply drops: full-area plies overhang shorter substrates and need an unsupported curved cover transition. The gallery depicts the base surface and authored schedule. Use the developed companion for station sampling.Cylindrical panel · radius 1219.2 mm · 957.6 mm arc × 609.6 mm axial · 9 plies · 1.234 mm nominal · Table 3, p.14: [30/-45/-30/45/90/45/-30/-45/30] at the end, [30/-30/90/-30/30] in the acreage-45°-30°30°45°90°Cylinder radius 48.0 in / 1219.2 mm (8-ft diameter)PUBLISHEDCylinder length 100 in / 2540 mmPUBLISHEDModelled axial extent from one cylinder end 24 in / 609.6 mmCHOSENSector angle 45deg (1/8 of the shell)CHOSEN
NASA/TM-20205008667Flat tool 957.6 × 609.6 mm · 9 plies · 1.234 mm nominal · Table 3, p.14: six bands from [30/-45/-30/45/90/45/-30/-45/30] to [30/-30/90/-30/30]-45°-30°30°45°90°Cylinder radius 48.0 in / 1219.2 mm (8-ft diameter)PUBLISHEDCylinder length 100 in / 2540 mmPUBLISHEDModelled axial extent from one cylinder end 24 in / 609.6 mmCHOSENSector angle 45deg (1/8 of the shell)CHOSEN
Imported CAD surface · 60 plies · 15.24 mm nominal · SS24, mirrored )S · preview shows the first 24-45°0°45°90°Stacking sequence and ply thickness SS24, 60 plies of 0.254 mmPUBLISHEDWing planform and section NACA 2412, 1800 mm root chord to 900 mm tip over a 4000 mm semi-spanCHOSEN
Synthetic starters
Editable examples. Most are synthetic: UD nominal ply thickness 0.195 mm, woven 0.26 mm, both design assumptions. The ones marked PUBLISHED take their stack and their ply thickness from a cited source instead — see each one's own note. Reproducing a published stack means the transcription is right and the laminate is internally consistent; it is not a claim that the part is producible, drapeable or qualified. Areal mass is ours in every case.