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Stiffening Sheet Metal by the Numbers

Making thin panels stiff, quiet and flat: plate deflection, buckling, flanges, wired edges, beads, stiffeners and vibration, with every number checked

Make thin sheet metal panels stiff, flat and quiet with numbers: plate deflection, thermal buckling, flanges, wired edges, beads, hat stiffeners and drumming.

9 chapters · About 91 minutes · Free to read · Intermediate mechanical design

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KEVOS® LibraryENGINEERINGREGIONTIMEPRODUCTStiffening SheetMetal by theNumbersKEVOS® ORIGINAL BOOK9 CHAPTERS

About this book

Thin sheet metal is cheap, light and easy to cut and fold, and it is also floppy. A flat panel of 1.2 mm steel the size of a small door bows visibly when air pressure acts on it, pops in and out when someone leans on it, buckles when the sun warms one side of an enclosure, and drums when a fan or motor nearby runs at the wrong speed. The answer is rarely just thicker sheet. Stiffness grows with the cube of thickness but so does nothing else useful, and a thicker panel can still drum. The better answers are shape: flanges and hems at the edges, wired and curled rims, rolled beads, and light stiffeners attached where they do the most work.

This book puts numbers on each of those choices. It starts with the flat panel, its deflection, stress and the point where the simple formulas stop applying, then explains buckling and oil-canning, then works through edge treatments, beads and attached stiffeners. It ends with vibration, because a panel that passes a static check can still fail by drumming, and with the tests that confirm a finished panel does what the numbers said.

It suits mechanical designers and drafters who design enclosures, guards, covers, doors and ductwork, and fabrication engineers who must explain why one panel rattles and another does not. It assumes school algebra, the idea of a beam’s second moment of area, and a working knowledge of sheet metal folding. Sheet Metal Parts by the Numbers covers bends, flat patterns and hems as folding operations; this book is about what those features do for stiffness.

The running case

Every chapter follows one fictional panel. This is an illustration. A small machinery builder makes an enclosure for a dust-producing machine. The enclosure’s side panel, called SP-90 here, is 900 mm high and 600 mm wide, cut from 1.2 mm zinc-coated steel sheet and screwed at 150 mm pitch to a light frame. An extraction fan holds the inside of the enclosure about 250 Pa below the workshop. The fan runs at 1,450 rpm and the machine’s main motor at 2,880 rpm.

Customers have complained that the side panel bows inwards when the extraction runs, oil-cans with a bang when leaned on, and hums. The builder sets three targets for a redesign: a deflection of no more than 3 mm under 250 Pa, no panel mode within 25% of the fan or motor frequency, and no visible bowing when the enclosure stands in the sun. The business, the customers, the complaints and the mistakes are invented, and the material properties are illustrations, not a grade’s specified values. None describes KEVOS® work or a real product.

Source limits and professional responsibility

The plate, beam and vibration formulas in this book are classical results for ideal edge conditions and small deflections, and every calculation was checked by running it. Real panels sit between simply supported and clamped, carry residual stress from cutting, folding and welding, and are rarely perfectly flat, so the numbers are estimates that a test must confirm. Where a formula’s limits matter, the chapter says so.

The book is educational. Panels that guard people from moving parts, contain pressure, carry structural load or control noise exposure have their own Australian standards and work health and safety duties, and the design and acceptance of such panels is a matter for a competent engineer and the applicable requirements. The 1918 trade text listed in the references was used only as a map of edge treatments; nothing from it is reproduced.

Who this book is for

Mechanical designers, drafters and fabrication engineers who design sheet metal enclosures, covers, doors and ducts, and who need panels that do not bow, buckle, oil-can or drum.

What you will learn

  • Estimate the deflection and stress of a flat rectangular panel and know when small-deflection theory stops applying.
  • Explain why thin panels buckle and oil-can with tiny temperature differences, and design to avoid it.
  • Compare flanges, hems, wired edges, beads and attached stiffeners by stiffness, mass and forming strain.
  • Calculate a panel's natural frequencies and keep them clear of the machinery that excites them.
  • Test a finished panel for deflection and frequency and record the result against the design targets.

Inside this book

Chapters

  1. 01Why thin sheet bends so easilySee why a thin panel's stiffness depends on the cube of its thickness, put a number on how far a flat panel bows, and catch a thicker-sheet fix that adds mass but misses the target.
  2. 02Deflection and stress of a flat panelCalculate a rectangular panel's deflection and bending stress under pressure for supported and clamped edges, see why the short side governs, and catch a calculation that used the long side.
  3. 03Buckling, oil-canning and a few degrees of heatSee how small a compressive stress buckles a thin panel, why a degree of temperature difference can do it, how big the buckle gets, and catch an afternoon buckle blamed on the folder.
  4. 04Flanges, returns and hems: stiffening the edgeCalculate how much a folded return or lip stiffens a panel's edge, see why a flange stiffens the edge and not the middle, and catch returns added to cure a bow they could not touch.
  5. 05Openings, curls and wired edgesStiffen a free edge with a hem, curl, wired edge or flange, size the wire allowance three ways, find the corner radius a flanged opening needs, and catch corners that split.
  6. 06Beads, swages and crownsSize a rolled bead from its stiffness and its forming strain, lay out beads across the short span, use crowns and cross-breaks for stability, and catch beads that shortened the panel.
  7. 07Hat sections and attached stiffenersSize a hat-section stiffener with the panel acting as its flange, compare layouts by bay size, check the rivets' shear, and catch flat bars fitted flat that left the panel as soft as before.
  8. 08Natural frequencies and drummingCalculate a panel's natural frequencies, compare them with the fan and motor that excite it, see why stiffer is not always quieter, and catch a beaded panel tuned exactly to the fan.
  9. 09Choosing and testing a stiffened panelCompare every stiffening option against all the targets at once, test the chosen panel for deflection, snap-through, heat and frequency, and catch a tap test done on the bench.

Apply This in Practice

Use these KEVOS® tools to try the method from this reading with your own numbers.

References and source notes

The manuscript and worked examples are original KEVOS® writing. References inform particular concepts; their authors do not endorse this book. Web references were consulted on 26 October 2026.

  • James S. Daugherty (Frederick J. Drake & Co., Chicago). Essentials of Sheet Metal Work and Pattern Drafting (1918). Supplied public-domain trade-school text, read as a subject map of edge treatments: hems, wired edges and their allowances, beading and burring. Its two shop rules for wire allowance are stated in Chapter 5 and compared with a geometric estimate. No passages, figures, tables or exercises are reproduced.
  • S. Timoshenko and S. Woinowsky-Krieger (McGraw-Hill). Theory of Plates and Shells, 2nd edition (1959). Source of the small-deflection coefficients for uniformly loaded rectangular plates with simply supported and clamped edges used in Chapters 1, 2 and 7, and of the flexural rigidity D.
  • S. Timoshenko and J. M. Gere (McGraw-Hill). Theory of Elastic Stability, 2nd edition (1961). Source of the critical buckling stress of simply supported plates under uniaxial and biaxial compression used in Chapter 3.
  • R. D. Blevins (Van Nostrand Reinhold). Formulas for Natural Frequency and Mode Shape (1979). Reference for the natural frequencies of a simply supported rectangular plate and a simply supported beam used in Chapter 8.
  • W. C. Young and R. G. Budynas (McGraw-Hill). Roark's Formulas for Stress and Strain, 7th edition (2002). General reference for beam deflection and for the limits of small-deflection plate formulas discussed in Chapters 2 to 4. No tables are reproduced.
  • Standards Australia. AS 1397 Continuous hot-dip metallic coated steel sheet and strip (edition as called up). Named by number and scope as the Australian product standard for the zinc-coated sheet in the running case. No values are quoted from it; the case's material properties are illustrations.
  • Safe Work Australia. Noise: overview (2026). Reference for the Australian approach to managing workplace noise, cited in Chapter 8 where drumming panels add to machine noise.
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