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21/04/2026

๐—•๐—น๐—ฎ๐˜€๐˜ ๐—ช๐—ฎ๐˜ƒ๐—ฒ๐˜€ ๐—ฎ๐—ป๐—ฑ ๐—™๐—ฟ๐—ฎ๐—ด๐—บ๐—ฒ๐—ป๐˜ ๐—œ๐—บ๐—ฝ๐—ฎ๐—ฐ๐˜๐˜€ ๐—–๐—ผ๐—บ๐—ฏ๐—ถ๐—ป๐—ฒ๐—ฑ

In this simulation, both the ๐—ฏ๐—น๐—ฎ๐˜€๐˜ ๐˜„๐—ฎ๐˜ƒ๐—ฒ and ๐—ฝ๐—ฟ๐—ฒ๐—ณ๐—ผ๐—ฟ๐—บ๐—ฒ๐—ฑ ๐—ณ๐—ฟ๐—ฎ๐—ด๐—บ๐—ฒ๐—ป๐˜๐˜€ are modelled together. As the detonation occurs, the blast wave propagates outward while fragments are simultaneously accelerated and dispersed, creating a highly directional and non-uniform loading environment.

If you are working in ๐˜ฃ๐˜ญ๐˜ข๐˜ด๐˜ต ๐˜ฑ๐˜ณ๐˜ฐ๐˜ต๐˜ฆ๐˜ค๐˜ต๐˜ช๐˜ฐ๐˜ฏ, ๐˜ช๐˜ฎ๐˜ฑ๐˜ข๐˜ค๐˜ต ๐˜ฆ๐˜ฏ๐˜จ๐˜ช๐˜ฏ๐˜ฆ๐˜ฆ๐˜ณ๐˜ช๐˜ฏ๐˜จ, or ๐˜ด๐˜ต๐˜ณ๐˜ถ๐˜ค๐˜ต๐˜ถ๐˜ณ๐˜ข๐˜ญ ๐˜ณ๐˜ฆ๐˜ด๐˜ช๐˜ญ๐˜ช๐˜ฆ๐˜ฏ๐˜ค๐˜ฆ, incorporating this type of coupled analysis can provide much deeper insight into real-world scenarios. This example will be discussed in my upcoming workshop: ๐™„๐™ข๐™ฅ๐™–๐™˜๐™ฉ ๐™–๐™ฃ๐™™ ๐™‹๐™š๐™ฃ๐™š๐™ฉ๐™ง๐™–๐™ฉ๐™ž๐™ค๐™ฃ๐™จ ๐˜ฝ-๐™„๐™„. More details here ๐Ÿ”—๐Ÿ‘‰: [https://lnkd.in/gSj4Yv7X]

๐Ÿš€ ๐—•๐—ฎ๐—ฐ๐—ธ ๐—ฏ๐˜† ๐—ฝ๐—ผ๐—ฝ๐˜‚๐—น๐—ฎ๐—ฟ ๐—ฑ๐—ฒ๐—บ๐—ฎ๐—ป๐—ฑ! ๐Ÿš€After a two-years wait, ๐˜๐˜ฎ๐˜ฑ๐˜ข๐˜ค๐˜ต ๐˜ข๐˜ฏ๐˜ฅ ๐˜—๐˜ฆ๐˜ฏ๐˜ฆ๐˜ต๐˜ณ๐˜ข๐˜ต๐˜ช๐˜ฐ๐˜ฏ๐˜ด ๐˜ธ๐˜ช๐˜ต๐˜ฉ ๐˜“๐˜š-๐˜‹๐˜ ๐˜•๐˜ˆ returns, the most sought-after w...
07/04/2026

๐Ÿš€ ๐—•๐—ฎ๐—ฐ๐—ธ ๐—ฏ๐˜† ๐—ฝ๐—ผ๐—ฝ๐˜‚๐—น๐—ฎ๐—ฟ ๐—ฑ๐—ฒ๐—บ๐—ฎ๐—ป๐—ฑ! ๐Ÿš€

After a two-years wait, ๐˜๐˜ฎ๐˜ฑ๐˜ข๐˜ค๐˜ต ๐˜ข๐˜ฏ๐˜ฅ ๐˜—๐˜ฆ๐˜ฏ๐˜ฆ๐˜ต๐˜ณ๐˜ข๐˜ต๐˜ช๐˜ฐ๐˜ฏ๐˜ด ๐˜ธ๐˜ช๐˜ต๐˜ฉ ๐˜“๐˜š-๐˜‹๐˜ ๐˜•๐˜ˆ returns, the most sought-after workshop in my lineup.

If you're looking to sharpen your skills in high-velocity impact modelling, this hands-on session is built for you. You'll explore the dynamic world of structural simulation using LS-DYNA, one of the most powerful tools for nonlinear analysis.

Whether you're an experienced FEA practitioner or just getting started, this workshop will help you build confidence, deepen your understanding, and take your modelling capabilities to the next level.

Here's what's on the agenda:

๐Ÿ”น Impact Response of Automotive Crash Box
๐Ÿ”น Projectile Impact on Ceramics Plate (2D Analysis)
๐Ÿ”น High Velocity Impact on a Woven Fabric Target
๐Ÿ”น Combined Fragment Impact and Blast Loading

๐Ÿ“… Workshop Details:

๐Ÿ”น Platform: Microsoft Teams
๐Ÿ”น Date: 27 - 30 Apr 2026 (Monday - Thursday)
๐Ÿ”น Time: 06:00 am - 09:00 am (GMT)

๐Ÿ’ฐ Participation Fees:

๐Ÿ”น Normal Price: USD260
๐Ÿ”น Student Price: USD160

Elevate your skills, and secure your seat and gain advanced expertise in high-velocity impact modeling with LS-DYNA.

๐Ÿ”— Register here: [https://forms.gle/TyLavKNcthsde2MZ6]

Don't miss out on this opportunity to expand your knowledge and enhance your career prospects. See you in class! ๐ŸŒŸ

18/12/2025

๐Ÿ’ฅ๐Ÿ’ฃ ๐—”๐—ป ๐—˜๐—ณ๐—ณ๐—ถ๐—ฐ๐—ถ๐—ฒ๐—ป๐˜ ๐—ช๐—ฎ๐˜† ๐˜๐—ผ ๐— ๐—ผ๐—ฑ๐—ฒ๐—น ๐—•๐—น๐—ฎ๐˜€๐˜ ๐—Ÿ๐—ผ๐—ฎ๐—ฑ๐—ถ๐—ป๐—ด ๐Ÿ’ฃ๐Ÿ’ฅ

In our numerical showcase [https://lnkd.in/gHaz3SsT], we emphasized the importance of ๐˜€๐—ถ๐—บ๐—ฝ๐—น๐—ถ๐—ณ๐˜†๐—ถ๐—ป๐—ด and ๐—ฟ๐—ฒ๐—ฑ๐˜‚๐—ฐ๐—ถ๐—ป๐—ด the problem ๐—ฏ๐—ฒ๐—ณ๐—ผ๐—ฟ๐—ฒ ๐—ท๐˜‚๐—บ๐—ฝ๐—ถ๐—ป๐—ด into ๐—ฑ๐—ฒ๐˜๐—ฎ๐—ถ๐—น๐—ฒ๐—ฑ ๐—บ๐—ผ๐—ฑ๐—ฒ๐—น๐—ถ๐—ป๐—ด. Building on that mindset, today we share an ๐—ฒ๐—ณ๐—ณ๐—ถ๐—ฐ๐—ถ๐—ฒ๐—ป๐˜ ๐˜„๐—ฎ๐˜† to ๐—บ๐—ผ๐—ฑ๐—ฒ๐—น ๐—ฏ๐—น๐—ฎ๐˜€๐˜ ๐—น๐—ผ๐—ฎ๐—ฑ๐—ถ๐—ป๐—ด, focusing on structural response without the need to explicitly simulate the explosion itself.

*๐—Ÿ๐—ข๐—”๐——_๐—•๐—Ÿ๐—”๐—ฆ๐—ง ๐—˜๐—ก๐—›๐—”๐—ก๐—–๐—˜๐—— (๐—Ÿ๐—•๐—˜) is an empirical blast loading option in LS-DYNA that applies air-blast pressures directly to structures without explicitly modeling the explosive or the surrounding air. Based on ๐—–๐—ข๐—ก๐—ช๐—˜๐—ฃ (Conventional Weapons Effects Program), it is widely used for efficient, engineering-level blast analyses where structural response is the primary focus ๐ŸŽฏ๐Ÿ’ฅ.

In this numerical showcase, which was featured in our recent ๐˜“๐˜š-๐˜‹๐˜ ๐˜•๐˜ˆ ๐˜ธ๐˜ฐ๐˜ณ๐˜ฌ๐˜ด๐˜ฉ๐˜ฐ๐˜ฑ on 29-30 Nov & 6-7 Dec ๐ŸŽ“๐Ÿง  (details here: [https://lnkd.in/gABJnTnq]), three different blast source types were demonstrated. These include:
๐Ÿ’ฅ Type 2: ๐˜€๐—ฝ๐—ต๐—ฒ๐—ฟ๐—ถ๐—ฐ๐—ฎ๐—น air burst ๐ŸŒ
๐Ÿ’ฅ Type 3: air burst from ๐—ฎ ๐—บ๐—ผ๐˜ƒ๐—ถ๐—ป๐—ด ๐—ป๐—ผ๐—ป-๐˜€๐—ฝ๐—ต๐—ฒ๐—ฟ๐—ถ๐—ฐ๐—ฎ๐—น ๐˜„๐—ฎ๐—ฟ๐—ต๐—ฒ๐—ฎ๐—ฑ ๐Ÿš€
๐Ÿ’ฅ Type 4: air burst with ๐—ด๐—ฟ๐—ผ๐˜‚๐—ป๐—ฑ ๐—ฟ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป๐˜€ ๐ŸŒ

A lesser-known capability is that blast pressure fields can also be visualized by introducing a plane of shell elements ๐Ÿ“ˆ๐Ÿ“, as shown in this example. All three cases were set up with the same ๐˜€๐—ฐ๐—ฎ๐—น๐—ฒ๐—ฑ ๐—ฑ๐—ถ๐˜€๐˜๐—ฎ๐—ป๐—ฐ๐—ฒ to enable a fair comparison. โš–๏ธ

The incident pressure histories reveal clear differences:
๐ŸŒ Type 2 strictly follows the ๐—ถ๐—ฑ๐—ฒ๐—ฎ๐—น open-air blast overpressure curve ๐Ÿ“ˆ.
๐Ÿš€ Type 3 shows a ๐—ต๐—ถ๐—ด๐—ต๐—ฒ๐—ฟ ๐—ฝ๐—ฒ๐—ฎ๐—ธ overpressure and ๐—ฒ๐—ฎ๐—ฟ๐—น๐—ถ๐—ฒ๐—ฟ ๐—ฎ๐—ฟ๐—ฟ๐—ถ๐˜ƒ๐—ฎ๐—น โฑ๏ธ, despite having the same scaled distance, which is due the directional effects of a non-symmetric blast source
๐ŸŒ Type 4 exhibits a distinct second pressure peak, originating from ๐—ด๐—ฟ๐—ผ๐˜‚๐—ป๐—ฑ ๐—ฟ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป effects ๐ŸŒโฌ†๏ธ.

The plate subjected to Type 4 loading experiences the ๐—น๐—ฎ๐—ฟ๐—ด๐—ฒ๐˜€๐˜ ๐—บ๐—ฎ๐˜…๐—ถ๐—บ๐˜‚๐—บ ๐—ฑ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป ๐Ÿ“โฌ†๏ธ, even though its peak overpressure is lower than that of Type 3. This behavior is explained by its ๐—ต๐—ถ๐—ด๐—ต๐—ฒ๐—ฟ ๐—ถ๐—บ๐—ฝ๐˜‚๐—น๐˜€๐—ฒ, which is the area under the pressure-time curve ๐Ÿ“Š. It is also observed that the deflection response for Type 3 initiates earlier, consistent with its ๐—ฒ๐—ฎ๐—ฟ๐—น๐—ถ๐—ฒ๐—ฟ blast arrival time โฑ๏ธ.

However, it is important to understand the ๐—น๐—ถ๐—บ๐—ถ๐˜๐—ฎ๐˜๐—ถ๐—ผ๐—ป๐˜€ of this approach. The ๐—Ÿ๐—•๐—˜ method does not model air, detonation physics, or confined blast effects ๐Ÿšซ๐Ÿ’จ๐Ÿ”ฅ. For near-field explosions, enclosed environments, or fluidโ€“structure interaction, higher-fidelity methods such as ๐—”๐—Ÿ๐—˜, ๐—ฆ๐—ฃ๐—›, or ๐—ฃ๐—•๐—  should be used instead. These advanced topics were covered in our ๐˜‰๐˜ญ๐˜ข๐˜ด๐˜ต ๐˜ข๐˜ฏ๐˜ฅ ๐˜Œ๐˜น๐˜ฑ๐˜ญ๐˜ฐ๐˜ด๐˜ช๐˜ฐ๐˜ฏ๐˜ด ๐˜ธ๐˜ฐ๐˜ณ๐˜ฌ๐˜ด๐˜ฉ๐˜ฐ๐˜ฑ held in September ๐Ÿ“…๐Ÿ’ฅ (workshop details here: [https://lnkd.in/gtyFT2Ci]).

02/12/2025

Can you use implicit solver for dynamic analysis?

Yes, you absolutely can. In fact, in some situations it is the better choice.

This is one of the examples covered in my ongoing LS-DYNA workshop (28โ€“29 Nov & 6โ€“7 Dec). For more details: [https://lnkd.in/gABJnTnq]

28/11/2025

Why Do We Use Different Projectile Types in High-Velocity Impact Tests?

Researchers employ different projectile types depending on the physical phenomena they aim to study and the industry application, such as aircraft bird-strike analysis, armor and protective structure testing, and evaluation of fragmentation threats.

In numerical showcase, all impacts were performed on a 3.0 mm thick aluminum plate, with an effective impact window of 300 ร— 300 mm. *๐— ๐—”๐—ง_๐— ๐—ข๐——๐—œ๐—™๐—œ๐—˜๐——_๐—๐—ข๐—›๐—ก๐—ฆ๐—ข๐—ก_๐—–๐—ข๐—ข๐—ž was adopted in order to capture strain-rate effects, thermal softening, and damage evolution under high-speed loading conditions.

To highlight the role of projectile rigidity, density, and failure mechanics, three projectiles representing different classes of impact threats were selected: ๐—ฆ๐—ผ๐—ณ๐˜ ๐—ฃ๐—ฟ๐—ผ๐—ท๐—ฒ๐—ฐ๐˜๐—ถ๐—น๐—ฒ (Bird-like Material), ๐—™๐—ฟ๐—ฎ๐—ด๐—บ๐—ฒ๐—ป๐˜ ๐—ฆ๐—ถ๐—บ๐˜‚๐—น๐—ฎ๐˜๐—ถ๐—ป๐—ด ๐—ฃ๐—ฟ๐—ผ๐—ท๐—ฒ๐—ฐ๐˜๐—ถ๐—น๐—ฒ (FSP), ๐Ÿณ.๐Ÿต๐Ÿฎร—๐Ÿฏ๐Ÿฏ๐—บ๐—บ ๐—ž๐˜‚๐—ฟ๐˜‡ (Ballistic Round).

I. Soft Projectile: A Dent without Pe*******on

The soft spherical projectile causes local deformation on the plate but does not perforate it. This response is typical of bird-strike-type impacts, where the projectile behaves more like a fluid than a solid at high velocity.

The projectile undergoes hydrodynamic spreading, flattening and flowing across the impact surface. Energy is distributed over a large area and longer duration, reducing local stress concentration.

II. 7.92ร—33 mm Kurz: Efficient Pe*******on With Lower Exit Velocity

The ballistic round perforates the aluminum plate, demonstrating efficient pe*******on but with a lower exit velocity compared to the FSP.

This is because the projectileโ€™s pointed or ogive-shaped nose promotes efficient pe*******on by reducing resistance and concentrating stress at the leading edge. As a result, the ballistic round undergoes a smaller kinetic energy drop during perforation than the FSP. However, it also has lower mass than the FSP.

III. Fragment Simulating Projectile: Pe*******on With the Highest Exit Velocity

The FSP also penetrates the plate, but with the highest exit velocity of all rigid projectiles in this study. The FSP is a high-mass, high-density, hardened projectile designed for repeatable ballistic testing.

Its simple cylindrical geometry causes greater resistance and a larger drop in kinetic energy during pe*******on compared to the ballistic round. The plate typically fails through shear plugging or localized petaling, consistent with rigid-body impacts.

___________________________________________________________

Understanding how different projectile types influence failure patterns and the effect they have on pe*******on, perforation, and energy absorption is essential for interpreting high-velocity impact behaviour with confidence.

Modelling high-velocity impact on aluminum plates will be one of the key topics in our LS-DYNA workshop this weekend and the following one. Follow the link in the comment below for more details.

10/11/2025

๐Ÿ›ข๏ธ๐Ÿ—๏ธ ๐—œ๐—ป๐˜๐—ฟ๐—ผ๐—ฑ๐˜‚๐—ฐ๐˜๐—ถ๐—ผ๐—ป ๐˜๐—ผ ๐—ฃ๐—ถ๐—ฝ๐—ฒ๐—น๐—ถ๐—ป๐—ฒ ๐—•๐—ฒ๐—ป๐—ฑ๐—ถ๐—ป๐—ด ๐Ÿ“Š๐Ÿ”

In this showcase, a ๐—ต๐—ผ๐—ฟ๐—ถ๐˜‡๐—ผ๐—ป๐˜๐—ฎ๐—น ๐—ฝ๐—ถ๐—ฝ๐—ฒ๐—น๐—ถ๐—ป๐—ฒ (with L = 2.5 m, DN = 0.4 m, t = 10 mm) is fully fixed at one end and subjected to a vertical load at the free end, a classic cantilever beam bending problem.

Three FE models were considered:-
๐Ÿ”ต ๐—•๐—ฒ๐—ฎ๐—บ ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ (๐—˜๐—Ÿ๐—™๐—ข๐—ฅ๐—  = ๐Ÿฑ): Belytschko-Schwer tubular beam with cross-section integration)
๐ŸŸข ๐—ฆ๐—ต๐—ฒ๐—น๐—น ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ (๐—˜๐—Ÿ๐—™๐—ข๐—ฅ๐—  = ๐Ÿฎ): Belytschko-Tsay shell element)
๐Ÿ”ด ๐—ฆ๐—ผ๐—น๐—ถ๐—ฑ ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ (๐—˜๐—Ÿ๐—™๐—ข๐—ฅ๐—  = -๐Ÿญ): 8-point hexahedral formulation optimized for poor aspect ratios)

The ๐—น๐—ผ๐—ฎ๐—ฑโ€“๐—ฑ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป comparison shows a good agreement between all models and the analytical solution in the ๐—ฒ๐—น๐—ฎ๐˜€๐˜๐—ถ๐—ฐ ๐—ฟ๐—ฎ๐—ป๐—ด๐—ฒ. Interestingly, the beam element model displays a ๐—ฏ๐—ถ๐—น๐—ถ๐—ป๐—ฒ๐—ฎ๐—ฟ ๐—ฏ๐—ฒ๐—ต๐—ฎ๐˜ƒ๐—ถ๐—ผ๐—ฟ, likely due to having only one element through the cross-section, which causes a relatively sharp transition from elastic to plastic response as that single integration zone forms a ๐—ฝ๐—น๐—ฎ๐˜€๐˜๐—ถ๐—ฐ ๐—ต๐—ถ๐—ป๐—ด๐—ฒ.

Meanwhile, the shell and solid models capture a ๐˜€๐—บ๐—ผ๐—ผ๐˜๐—ต๐—ฒ๐—ฟ ๐˜๐—ฟ๐—ฎ๐—ป๐˜€๐—ถ๐˜๐—ถ๐—ผ๐—ป and more gradual plastic development, consistent with physical expectations.

The contours of von-Mises effective stress, Y-stress (which is the bending axis), and the effective plastic strain (all taken from the ๐˜€๐—ผ๐—น๐—ถ๐—ฑ ๐—ฒ๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ ๐—บ๐—ผ๐—ฑ๐—ฒ๐—น) are shown on the right.

During the initial stage of loading, up to approximately ๐Ÿญ๐Ÿณ ๐—บ๐—บ ๐—ผ๐—ณ ๐—ฑ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป, the pipeline exhibits ๐—ฏ๐—ฒ๐—ป๐—ฑ๐—ถ๐—ป๐—ด ๐˜€๐˜๐—ฟ๐—ฒ๐˜€๐˜€๐—ฒ๐˜€ but ๐—ป๐—ผ ๐—ฒ๐—ณ๐—ณ๐—ฒ๐—ฐ๐˜๐—ถ๐˜ƒ๐—ฒ ๐—ฝ๐—น๐—ฎ๐˜€๐˜๐—ถ๐—ฐ ๐˜€๐˜๐—ฟ๐—ฎ๐—ถ๐—ป, indicating that the response remains purely elastic.

As the ๐—น๐—ผ๐—ฎ๐—ฑโ€“๐—ฑ๐—ฒ๐—ณ๐—น๐—ฒ๐—ฐ๐˜๐—ถ๐—ผ๐—ป ๐—ฐ๐˜‚๐—ฟ๐˜ƒ๐—ฒ of the solid model begins to ๐—ฑ๐—ฒ๐˜ƒ๐—ถ๐—ฎ๐˜๐—ฒ from the ๐—น๐—ถ๐—ป๐—ฒ๐—ฎ๐—ฟ ๐—ฎ๐—ป๐—ฎ๐—น๐˜†๐˜๐—ถ๐—ฐ๐—ฎ๐—น ๐—ฝ๐—ฟ๐—ฒ๐—ฑ๐—ถ๐—ฐ๐˜๐—ถ๐—ผ๐—ป, the onset of plastic deformation becomes evident, with ๐—น๐—ผ๐—ฐ๐—ฎ๐—น๐—ถ๐˜‡๐—ฒ๐—ฑ ๐—ฝ๐—น๐—ฎ๐˜€๐˜๐—ถ๐—ฐ ๐˜€๐˜๐—ฟ๐—ฎ๐—ถ๐—ป๐˜€ gradually developing near the ๐—ณ๐—ถ๐˜…๐—ฒ๐—ฑ ๐—ฒ๐—ป๐—ฑ of the pipeline.

This will be one of the examples covered in my upcoming workshop on ๐Ÿฎ๐Ÿต - ๐Ÿฏ๐Ÿฌ ๐—ก๐—ผ๐˜ƒ & ๐Ÿฒ - ๐Ÿณ ๐——๐—ฒ๐—ฐ. ๐Ÿ‘‰ More about this workshop, check the link in the comment.


๐Ÿ—“๏ธ It's November already and the year is coming to an end, but it's ๐˜ฏ๐˜ฐ๐˜ต ๐˜ต๐˜ฐ๐˜ฐ ๐˜ญ๐˜ข๐˜ต๐˜ฆ ๐˜ต๐˜ฐ ๐˜ฃ๐˜ฆ๐˜จ๐˜ช๐˜ฏ ๐˜บ๐˜ฐ๐˜ถ๐˜ณ ๐˜ซ๐˜ฐ๐˜ถ๐˜ณ๐˜ฏ๐˜ฆ๐˜บ ๐˜ธ๐˜ช๐˜ต๐˜ฉ ๐˜๐˜ช๐˜ฏ๐˜ช๐˜ต๐˜ฆ ๐˜Œ๐˜ญ๐˜ฆ๐˜ฎ๐˜ฆ...
06/11/2025

๐Ÿ—“๏ธ It's November already and the year is coming to an end, but it's ๐˜ฏ๐˜ฐ๐˜ต ๐˜ต๐˜ฐ๐˜ฐ ๐˜ญ๐˜ข๐˜ต๐˜ฆ ๐˜ต๐˜ฐ ๐˜ฃ๐˜ฆ๐˜จ๐˜ช๐˜ฏ ๐˜บ๐˜ฐ๐˜ถ๐˜ณ ๐˜ซ๐˜ฐ๐˜ถ๐˜ณ๐˜ฏ๐˜ฆ๐˜บ ๐˜ธ๐˜ช๐˜ต๐˜ฉ ๐˜๐˜ช๐˜ฏ๐˜ช๐˜ต๐˜ฆ ๐˜Œ๐˜ญ๐˜ฆ๐˜ฎ๐˜ฆ๐˜ฏ๐˜ต ๐˜ˆ๐˜ฏ๐˜ข๐˜ญ๐˜บ๐˜ด๐˜ช๐˜ด!!

If youโ€™ve always wanted to learn ๐—Ÿ๐—ฆ-๐——๐—ฌ๐—ก๐—”, this is your chance to close 2025 strong and step confidently into the new year with a solid foundation in ๐—™๐—ถ๐—ป๐—ถ๐˜๐—ฒ ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ ๐—”๐—ป๐—ฎ๐—น๐˜†๐˜€๐—ถ๐˜€ (๐—™๐—˜๐—”).

๐ŸŽ“ Join our ๐—ผ๐—ป๐—น๐—ถ๐—ป๐—ฒ ๐˜„๐—ผ๐—ฟ๐—ธ๐˜€๐—ต๐—ผ๐—ฝ: "๐—Ÿ๐—ฆ-๐——๐—ฌ๐—ก๐—” ๐—ถ๐—ป ๐—ฎ ๐—ก๐˜‚๐˜๐˜€๐—ต๐—ฒ๐—น๐—น", where we tackle the fundamentals of Finite Element Analysis with LS-DYNA. This event is designed especially for beginners, postgraduate students, and professionals eager to explore FEA through practical examples.

๐Ÿ“… ๐——๐—ฎ๐˜๐—ฒ๐˜€: 29 โ€“ 30 November & 6 โ€“ 7 December 2025
๐Ÿ•‘ ๐—ง๐—ถ๐—บ๐—ฒ: 2:00 PM โ€“ 4:00 PM (Malaysia Time / GMT+8)
๐Ÿ’ป ๐— ๐—ผ๐—ฑ๐—ฒ: Online (Live + Recorded Sessions)
๐Ÿ’ฐ ๐—™๐—ฒ๐—ฒ: USD120 (Standard) | USD75 (Students)

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๐Ÿ” ๐—ช๐—ต๐—ฎ๐˜ ๐—ฌ๐—ผ๐˜‚โ€™๐—น๐—น ๐—Ÿ๐—ฒ๐—ฎ๐—ฟ๐—ป

Through ๐—ณ๐—ผ๐˜‚๐—ฟ ๐—ฐ๐—ฎ๐—ฟ๐—ฒ๐—ณ๐˜‚๐—น๐—น๐˜† ๐—ฑ๐—ฒ๐˜€๐—ถ๐—ด๐—ป๐—ฒ๐—ฑ ๐—ฒ๐˜…๐—ฎ๐—บ๐—ฝ๐—น๐—ฒ๐˜€, youโ€™ll understand how to model, simulate, and analyze structures in LS-DYNA, from static bending to dynamic impact:
1๏ธโƒฃ Pipeline Bending Analysis โ€“ 1D, 2D, and 3D Modeling
2๏ธโƒฃ Buckling of Stiffened Panels โ€“ Modal vs Nonlinear Analysis
3๏ธโƒฃ Composite Targets under Impulsive Loading โ€“ Brittle and Ductile Material Models
4๏ธโƒฃ Projectile Impact on Circular Panel โ€“ Axisymmetric vs 3D Solid Modeling

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๐ŸŽฏ ๐—ž๐—ฒ๐˜† ๐—›๐—ถ๐—ด๐—ต๐—น๐—ถ๐—ด๐—ต๐˜๐˜€

โ— Step-by-step demonstrations
โ— Focus on modeling fundamentals and solver selection
โ— Real-world applications in structural, impact, and dynamic analysis
โ— Recordings available for all participants
โ— e-Certificate upon completion

____________________________________________________________

Seats are limited, donโ€™t miss this opportunity to learn LS-DYNA in a clear, structured way!

๐Ÿ‘‰ ๐—ฅ๐—ฒ๐—ด๐—ถ๐˜€๐˜๐—ฒ๐—ฟ ๐—ก๐—ผ๐˜„ and make your first (or next) step in FEA before 2025 ends.
๐Ÿ”— [https://lnkd.in/gJNgxPSw]

๐ŸŽ“ ๐—” ๐—•๐—ฒ๐—ด๐—ถ๐—ป๐—ป๐—ฒ๐—ฟโ€™๐˜€ ๐—ช๐—ผ๐—ฟ๐—ธ๐˜€๐—ต๐—ผ๐—ฝ: ๐—™๐—ถ๐—ป๐—ถ๐˜๐—ฒ ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ ๐—”๐—ป๐—ฎ๐—น๐˜†๐˜€๐—ถ๐˜€ ๐˜„๐—ถ๐˜๐—ต ๐—Ÿ๐—ฆ-๐——๐—ฌ๐—ก๐—”๐Ÿš€ Itโ€™s not too late to begin your journey with Finite Eleme...
03/11/2025

๐ŸŽ“ ๐—” ๐—•๐—ฒ๐—ด๐—ถ๐—ป๐—ป๐—ฒ๐—ฟโ€™๐˜€ ๐—ช๐—ผ๐—ฟ๐—ธ๐˜€๐—ต๐—ผ๐—ฝ: ๐—™๐—ถ๐—ป๐—ถ๐˜๐—ฒ ๐—˜๐—น๐—ฒ๐—บ๐—ฒ๐—ป๐˜ ๐—”๐—ป๐—ฎ๐—น๐˜†๐˜€๐—ถ๐˜€ ๐˜„๐—ถ๐˜๐—ต ๐—Ÿ๐—ฆ-๐——๐—ฌ๐—ก๐—”

๐Ÿš€ Itโ€™s not too late to begin your journey with Finite Element Analysis!

Join this ๐Ÿฐ-๐—ฑ๐—ฎ๐˜† ๐—ผ๐—ป๐—น๐—ถ๐—ป๐—ฒ ๐˜„๐—ผ๐—ฟ๐—ธ๐˜€๐—ต๐—ผ๐—ฝ designed for students, researchers, and professionals who want to learn ๐—Ÿ๐—ฆ-๐——๐—ฌ๐—ก๐—”, one of the worldโ€™s most powerful and versatile simulation tools for ๐˜€๐˜๐—ฟ๐˜‚๐—ฐ๐˜๐˜‚๐—ฟ๐—ฎ๐—น, ๐—ถ๐—บ๐—ฝ๐—ฎ๐—ฐ๐˜, ๐—ฎ๐—ป๐—ฑ ๐—ฑ๐˜†๐—ป๐—ฎ๐—บ๐—ถ๐—ฐ ๐—ฎ๐—ป๐—ฎ๐—น๐˜†๐˜€๐—ฒ๐˜€.

๐Ÿ—“๏ธ ๐——๐—ฎ๐˜๐—ฒ๐˜€: 29โ€“30 November & 6โ€“7 December 2025
๐Ÿ•‘ ๐—ง๐—ถ๐—บ๐—ฒ: 2:00 PM โ€“ 4:00 PM (Malaysia Time / GMT+8)
๐Ÿ’ป ๐— ๐—ผ๐—ฑ๐—ฒ: Online via Microsoft Teams (All sessions recorded)
๐Ÿ“œ ๐—ฒ-๐—–๐—ฒ๐—ฟ๐˜๐—ถ๐—ณ๐—ถ๐—ฐ๐—ฎ๐˜๐—ฒ ๐—ฃ๐—ฟ๐—ผ๐˜ƒ๐—ถ๐—ฑ๐—ฒ๐—ฑ

๐Ÿ’ฐ ๐—™๐—ฒ๐—ฒ๐˜€ (๐— ๐—ฎ๐—น๐—ฎ๐˜†๐˜€๐—ถ๐—ฎ):
โ€ข RM500 โ€“ Professional/Staff
โ€ข RM300 โ€“ Student (with valid ID)

โœจ ๐—ช๐—ต๐—ฎ๐˜ ๐—ฌ๐—ผ๐˜‚โ€™๐—น๐—น ๐—Ÿ๐—ฒ๐—ฎ๐—ฟ๐—ป:
โœ” Fundamentals of Finite Element Modeling
โœ” Differences between 1D, 2D & 3D simulations
โœ” Implicit vs Explicit Solvers
โœ” Static & Dynamic Case Studies
โœ” Real-world examples from structural and impact simulations

๐Ÿ”— Register now: [https://forms.gle/78T89gCtgLjq3Jkb6]
Seats are limited, donโ€™t miss this opportunity to learn LS-DYNA in a clear and practical way.

๐Ÿ”— For more information, check out our LinkedIn post: [https://lnkd.in/gABJnTnq]

21/10/2025

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