In order to perform structural analysis required to design aerospace parts that will meet service and regulatory requirements, it is necessary to understand the manufacturing processes involved, the mechanical properties of the materials produced, and the effect of defects on the static strength, fatigue, and fracture properties of those materials.
Not all metal additive manufacturing (AM) is created equal. Powder bed fusion (PBF) and direct energy deposition (DED) may both melt metal layer by layer, but they yield fundamentally different microstructures, surface finishes, and defect modes. For structural engineers, this isn't just a manufacturing detail—it's a design-critical distinction.
Structural engineers can't treat AM parts generically. Process selection drives design allowables and analysis assumptions. The way energy is delivered, how powder is consolidated, and the thermal history experienced by each layer all cascade into the mechanical properties we rely on for certification and service life prediction.
Understanding how each process forms and consolidates metal is the first step toward building accurate models and predictions.
Powder bed fusion processes involve the fusion of thin layers of metallic powder using either a laser or electron beam. In selective laser melting (SLM), a laser projects along a defined path, melting a thin layer of powder. After melting the required geometry in the build plane, an additional layer of powder is applied and subsequently melted until the part is complete. The build chamber is filled with an inert gas, such as argon, to prevent oxidation. Electron beam melting (EBM) operates similarly but uses an electron beam in a vacuum chamber instead of a laser.
PBF methods result in parts with fine resolution and high quality, making them suitable for use in the aerospace industry. However, as a consequence of this detail and quality, PBF processes can be slow and expensive.
The structural engineer must remember: PBF gives you precision, but it demands process discipline. Small parameter variations create large property scatter.
Direct energy deposition is another technique for melting metal powder to manufacture a part. However, DED does not use a bed of powder like PBF. Instead, DED injects metal powder or wire directly into the laser beam and deposits the melted metal onto a substrate. This fundamental difference changes everything about the structural performance.
DED does not produce as fine detail compared to PBF processes, and typically requires post-build machining to meet dimensional and surface finish requirements. But one major advantage of DED is that it can be used for repairing and retrofitting manufactured parts—something PBF cannot easily accomplish.
The structural takeaway: DED trades geometric precision for scale and speed. It's built for repair, not for tolerance.
When we compare PBF and DED from a structural perspective, the differences become stark:
| Structural Consideration | Powder Bed Fusion (PBF) | Direct Energy Deposition (DED) |
|---|---|---|
| Surface finish | Excellent; minimal machining required | Rough; machining required for critical surfaces |
| Porosity tendency | Highly process-parameter sensitive | Lower porosity but higher microstructural variation |
| Anisotropy | Pronounced due to layer-by-layer melting and columnar grains | Slightly mitigated by higher heat input and coarser structure |
| Residual stress | High; requires HIP or stress relief treatment | Moderate; thermal gradients more diffuse |
| Defect types | Gas porosity, lack of fusion voids, keyhole defects | Unmelted regions, inclusions, distortion |
| Application sweet spot | Complex, small, high-precision parts | Large builds, repairs, cladding |
| Structural risk driver | Fine-scale defects drive fatigue initiation | Macro-defects drive distortion and property mismatch |
| Cost and speed | Slow and expensive | Faster and more economical for large parts |
The key insight: Different processes create different failure modes.
In PBF, you're fighting porosity—tiny spherical gas pores and irregular lack-of-fusion voids that become fatigue crack initiation sites. In DED, you're managing coarser microstructures and geometric imperfections that create stress concentrations and property gradients.
For both aluminum alloys and titanium alloys, laser scan speed and laser power are recognized as the most influential parameters for porosity level. But here's the counterintuitive reality: porosity increases for both relatively slow velocities and relatively fast velocities, and for both relatively low power levels and relatively high power levels.
At low velocities, the laser overheats the titanium, allowing keyhole pores and gas porosities to form. At high velocities, the laser cannot heat the titanium to a high enough temperature, resulting in lack-of-fusion pores. Similarly, low power levels create insufficient melting, while high power levels trigger keyhole instability and gas entrapment.
This creates a narrow processing window. Small deviations lead to large mechanical scatter—directly impacting fatigue design allowables. For the structural engineer, this means:
Both PBF and DED require fine control of energy density to avoid porosity and incomplete fusion. The difference is that PBF's smaller melt pool and faster cooling make it more sensitive to parameter drift, while DED's larger thermal mass provides more process forgiveness—at the cost of geometric precision.
Certification authorities view AM processes as special processes—requiring validated parameters and post-process verification. This isn't just bureaucracy; it reflects the fundamental reality that AM parts are inseparable from the process that made them.
Structural substantiation must link: process → defect → property → performance.
This means:
The practical takeaway: choosing PBF vs. DED isn't just about how fast you can build the part or how smooth the surface will be. It determines whether your structural analysis will be dominated by micro-defect statistics or macro-geometry deviations. It decides whether heat treatment will be mandatory or optional. It dictates what your supply chain qualification process looks like.
Knowledge of the manufacturing process, the mechanical properties of the materials, and the effect of defects is necessary to develop the structural analysis methods and design data required to support the goal of making metal additive manufacturing as common and reliable as modern subtractive and forming processes.
PBF and DED give engineers two very different toolsets. One trades speed for precision; the other trades tolerance for scale. But both require the same structural discipline—understanding how process physics translate into material behavior.
The laser's path becomes the grain structure. The cooling rate becomes the residual stress. The scan strategy becomes the defect distribution. And all of these become the inputs to your stress analysis, your fatigue prediction, and your damage tolerance assessment.
The future of aerospace AM depends on how well we bridge that gap between how we print and how we predict. Process selection is structural selection. Choose wisely.
For structural engineers working to qualify AM components for aerospace applications, understanding these process-structure-property relationships isn't optional—it's foundational. The part you analyze tomorrow was created by the laser path planned yesterday.
🔗 Download my full 2018 Master's Literature Review & Research Proposal: Structural Analysis of Porosity Effects in Aerospace Metal AM
This article draws from the literature review and research proposal I developed during my master's degree on porosity effects in aerospace metal additive manufacturing, with particular focus on the structural analysis methods required to predict performance in the presence of process-induced defects. The intersection of advanced manufacturing and structural integrity represents one of the most challenging and rewarding frontiers in aerospace engineering.
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