Sajjad Ahmad

Mr. Sajjad Ahmad

International Islamic University, Islamabad, Islamabad, Islāmābād, Pakistan
orcid

Research Focus & Metrics

Academic Career Length

8Years (2019-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 September 2023 in Materials Research Express
Verified
Journal Article
Open access
ARAdnan Rasheed
Adnan Rasheed
MHMuhammad Hussain
Muhammad Hussain
SUShafi Ullah
Shafi Ullah
ZAZeeshan Ahmad
Zeeshan Ahmad
HKHasnain Kakakhail
Hasnain Kakakhail
IKIlyas Khan
Ilyas Khan
Additive manufacturing (AM) technology has gained significant popularity, among which Fused Deposition Modeling (FDM) has emerged as the predominant technique for 3D printing. FDM offers the unique ability to achieve the desired and tailored engineering properties required for specific applications. This experimental study investigates the influence of varying FDM process parameters on the mechanical properties and highlights the optimal set of parameters for better tensile strength for a bi-layered composite of PLA-ABS (polylactic acid and acrylonitrile butadiene styrene). Also, it investigates the most-to-least influential printing parameters. Four process parameters were played out i.e., Infill density (50%, 75%, and 100%), number of layers (20,25 and 30), printing speed (20 mm sec−1, 40 mm sec−1, and 60 mm sec−1), and bed temperature (90 °C, 95 °C, and 100 °C), while keeping other parameters constant. Taguchi optimization technique was used for optimization and experiments were designed according to Taguchi orthogonal array L9 (3 4). After printing, the samples were evaluated for tensile properties and the results were analyzed. It is found that the infill density is the most influential parameter while bed temperature is the least influential. Infill density of 75%, 30 layers per part, a printing speed of 20 mm sec−1, and a bed temperature of 100 °C are the optimal set of parameters for better tensile strength. Alongside, percent elongation, printing time, and strength-to-weight ratio were also analyzed and correlated.

11 March 2022 in Materials
Verified
Journal Article
Open access
PDF file
Imtiaz Alam ShahImtiaz Alam Shah
Imtiaz Alam Shah
RKRafiullah Khan
Rafiullah Khan
Seyed Saeid Rahimian KoloorSeyed Saeid Rahimian Koloor
Seyed Saeid Rahimian Koloor
Michal PetrůMichal Petrů
Michal Petrů
Saeed BadshahSaeed Badshah
Saeed Badshah
MAMuhammad Amjad
Muhammad Amjad
In this study, the ballistic impact behavior of auxetic sandwich composite human body armor was analyzed using finite element analysis. The auxetic core of the armor was composed of discrete re-entrant unit cells. The sandwich armor structure consisted of a front panel of aluminum alloy (Al 7075-T6), UHMWPE (sandwich core), and a back facet of silicon carbide (SiC) bonded together with epoxy resin. Numerical simulations were run on Explicit Dynamics/Autodyne 3-D code. Various projectile velocities with the same boundary conditions were used to predict the auxetic armor response. These results were compared with those of conventional monolithic body armor. The results showed improved indentation resistance with the auxetic armor. Deformation in auxetic armor was observed greater for each of the cases when compared to the monolithic armor, due to higher energy absorption. The elastic energy dissipation results in the lower indentation in an auxetic armor. The armor can be used safely up to 400 m/s; being used at higher velocities significantly reduced the threat level. Conversely, the conventional monolithic modal does not allow the projectile to pass through at a velocity below 300 m/s; however, the back face becomes severely damaged at 200 m/s. At a velocity of 400 m/s, the front facet of auxetic armor was destroyed; however, the back facet was completely safe, while the monolithic panel did not withstand this velocity and was completely damaged. The results are encouraging in terms of resistance offered by the newly adopted auxetic armor compared to conventional monolithic armor.

Verified
Journal Article
Open access
PDF file
SAShoaib Ahmed
Shoaib Ahmed
RRRana Atta ur Rahman
Rana Atta ur Rahman
AAAwais Awan
Awais Awan
SASajjad Ahmad
Sajjad Ahmad
Waseem AkramWaseem Akram
Waseem Akram
Seyed Saeid Rahimian KoloorSeyed Saeid Rahimian Koloor
Seyed Saeid Rahimian Koloor
Friction stir welding (FSW) is one of the primary fabrication techniques for joining different components, and it has become popular, especially in aluminum alloy structures for marine applications. The welded joint with the friction stir process greatly depends on the process parameters, i.e., feed rate, rotational speed, and pin profile of the tool. In the current study, plates of aluminum 5451 alloy were joined by the FSW technique, and the Taguchi method was used to find the process parameters at an optimal level. The maximum value of tensile strength, i.e., 160.6907 MPa, was achieved using optimum welding conditions of a tool rotation speed of 1400, a feed rate of 18 mm/min, and the tool pin with threads. The maximum value of hardness, i.e., 81.056 HV, was achieved using optimum conditions of 1200 tool rotational speed and a feed rate of 18 mm/min with a tool pin profile having threads. In addition, the contribution in terms of the percentage of each input parameter was found by the analysis of variance (ANOVA). The ANOVA results revealed that the pin profile of the tool has the maximum contribution of 67.77% and 62.42% in achieving the optimum value of tensile strength and hardness, respectively. The study also investigated the joint efficiency of the friction stir welded joint, hardness at the weld zone, and metallography on FSW samples at the optimized level. The effectiveness and reliability of FSW joints for shipping industry applications can be observed by joint efficiency. That was investigated at optimum conditions, and it comes out to be 80.5%.

8 August 2023 in Journal of Materials Research and Technology
Verified
Journal Article
Open access
Waseem AkramWaseem Akram
Waseem Akram
RKRafiullah Khan
Rafiullah Khan
Michal PetrůMichal Petrů
Michal Petrů
MAMuhammad Amjad
Muhammad Amjad
KAKhalil Ahmad
Khalil Ahmad
Seyed Saeid Rahimian KoloorSeyed Saeid Rahimian Koloor
Seyed Saeid Rahimian Koloor

23 October 2019 in Materials
Verified
Journal Article
Open access
PDF file
SASajjad Ahmad
Sajjad Ahmad
Saeed BadshahSaeed Badshah
Saeed Badshah
IHIhsan Haq
Ihsan Haq
SMSuheel Abdullah Malik
Suheel Abdullah Malik
MAMuhammad Amjad
Muhammad Amjad
Mohd Nasir TAMINMohd Nasir TAMIN
Mohd Nasir TAMIN
Wire ropes undergo a fretting fatigue condition when subjected to axial and bending loads. The fretting behavior of wires are classified as line contact and trellis point of contact. The experimental study on the fatigue of wire ropes indicates that most of the failure occurs due to high localized stresses at trellis point of contact. A continuum damage mechanics approach was previously proposed to estimate the fatigue life estimation of wire ropes. The approach majorly depends on the high value of localized stresses as well as the micro-slippage occurs at the contact region. Finite element approach has been used to study radial and axial distribution of stresses and displacement in order to clearly understand the evolution of stresses and existence of relative displacements between neighboring wires under various loading and frictional conditions. The relative movements of contacting wires are more when friction is not considered. In the presence of friction, the relative movement occurs at the boundaries of the contact region. The location of microslip in the presence of friction is backed by the experimental observation stating the crack is initiated at or the outer boundary of the contact spot. The existence of slip is due to different displacement of outer and central wires.

14 April 2025 in Fatigue & Fracture of Engineering Materials & Structures
Verified
Journal Article
Closed access
SASajjad Ahmad
Sajjad Ahmad
SBSaeed Badshah
Saeed Badshah
MAMuhammad Amjad
Muhammad Amjad
SKSakhi Jan Khalil
Sakhi Jan Khalil
MIMuhammad Ibrahim
Muhammad Ibrahim
MTMohd Nasir Tamin
Mohd Nasir Tamin