{"title":"Sloshing Analysis of a Supersonic Fuel Tank of an Aircraft","authors":"F. Iqbal, A. Javed, A. Shahzad","doi":"10.1109/ICAEM53552.2021.9547074","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547074","url":null,"abstract":"This paper presents sloshing analysis of fuel in a supersonic aircraft's fuel tank. Sloshing can be defined as the movement of a fluid inside a moving tank. Sloshing phenomenon is of great significance since it is involved in various fields such as propellant slosh in rockets, aircraft, cargo ships and also the trucks that carry different type of fluids. Sloshing occurs when a fluid containing body suddenly accelerates or decelerates that in turn leads to unnecessary vibrations, flammability, noise and structural failure. To reduce the sloshing effects, anti-slosh baffles are employed in the fuel tanks or any other fluid containing body. Baffles are the obstructions installed inside the fuel tank that absorb the kinetic energy of the waves and reduce the sloshing impact by lowering down the momentum of generated waves. In this research, Volume of Fluid Model has been used for Computational Fluid Dynamics analysis. After the analytical and experimental validation of the model, free surface behavior of sloshed liquid has been analyzed under different operating conditions. For experimental results, a commonly used water tank has been used to track the liquid interface under the application of an external force. Effectiveness of baffles has been studied by calculating the pressure forces on the walls of a fuel tank for both baffled and an un-baffled tank. It has been observed that baffles reduce the pressure forces to almost one tenth in the present case. Reaction forces at the tank mounts have been calculated by carrying out structural analysis of the supersonic fuel tank. Settling time is the time required for the sloshing waves to damp down and the said time for different fill levels and excitation forces has been calculated in the present research. Different cases of acceleration and fuel-fill levels have been taken to study the varying sloshing forces with time. This paper presents a detailed sloshing analysis along with a qualitative and quantitative study that is supported by analytical and experimental results.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"51 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127535531","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Hassan Shuaib, Syed Irtiza Ali Shah, A. Haseeb, Malik Muhammad Awais
{"title":"Mathematical Modelling and Design of Hydraulic Actuator Control System using Dynamometer","authors":"Hassan Shuaib, Syed Irtiza Ali Shah, A. Haseeb, Malik Muhammad Awais","doi":"10.1109/ICAEM53552.2021.9547191","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547191","url":null,"abstract":"Among different kinds of actuators, pressure-driven ones are significant and utilized because of their high capacity to weight proportion. The most significant utilization of pressuredriven actuators is related to flywheels. Utilizing actuators in blend with flywheels empowers us to control rotational speed (RPMs) and force of any instrument in a successful way. Such constructions are frequently observed in mechanical arms, boats, and marines. In this study, the design and analysis of control actuators with the flywheel are presented. One such device is a dynamometer which gives quick input estimation about the extent and power applied. Demonstrating such a framework needs a brought together way to deal with speak to the nonlinear conduct qualities. The bond diagram model is ideal for this undertaking. Moreover, traditional PID control methodology is utilized to accomplish the necessary exactness and accuracy, which is straightforward, programmed, less tedious, and proficient. Reproductions and investigations on the actuator are completed to assess the adequacy of the proposed control technique. The dynamometer framework is utilized for the testing and assessment of engine and powertrain segments. So We can utilize can dynamometer sensors to accomplish a close loop control framework as an actuator in the flywheel. flywheels accessible for when the motor driveline needs to incorporate a latency incentive to coordinate with the airframe transmission. Most flywheels are provided mounted in an independent base casing. Be that as it may, for specific applications their systems can be used as half couplings Dynamometer has likewise been utilized as a fundamental device. The standard of the dynamometer will be able to retain the power of the car and gauge force and speed and decide the motor yield power or the powertrain power to adjust the force and speed.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"86 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114859922","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Design, Analysis and Topology Optimization of a Landing Gear Strut for a Quadcopter Upon Impact","authors":"Sabih Ahmad Khan, Zahid Mehmood, Zar Afshan","doi":"10.1109/ICAEM53552.2021.9547116","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547116","url":null,"abstract":"In this paper, a comprehensive approach for design, analysis, and topology optimization for a solid leaf spring landing gear of a quadcopter is presented. Landing gears are a critical structural part of an aircraft that support all up weight in static conditions and absorb kinetic energy in a form of impact loads during touch down. Complete designing along with the analysis of landing gear as per the governing principals and rules have been carried out such that it undertakes static load and impact load of the aerial vehicle having Gross Take-off Weight of 12 kg including the payload capacity of 9 kg. The work includes a comprehensive literature review, mathematical modeling of the strut, calculation of Impact force at static and dynamic conditions. Drop test dynamics has been explained thoroughly which is a prerequisite for experimental verification using drop test of the designed strut before its installation on aerial vehicle. Considering the maximum force encountered during landing, the design of the landing gear along with appropriate thickness has also been undertaken in SOLIDWORKS®. The numerical analysis of the model has been conducted using the continuum approach, considering continuous bodies. Similarly, to validate the proposed design and to determine the structural integrity of strut, finite element analysis has been carried out on landing gear assembly. The deformation, maximum stresses (Von-Mises, Principle Stress) and factor of safety have been computed using SOLIDWORKS®Simulation-Static. Moreover, three materials have been initially used, (Cold Rolled Steel, Al 7075- T6, Al 2024-T3). High strength to weight ration is a critical design consideration for any landing gear strut. The optimization parameter for the analysis is weight of the strut. Hence three optimum variants of the struts have also been proposed with 15%, 35%, 60% reduced weight of each without compromising the strength. The results indicate that the designed strut behaves efficiently meeting all the operational conditions.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132965592","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Ghulam Muhay Ud Din, Nusrat Husain, Ashraf Yahya, Z. Arfeen
{"title":"Mathematical Analysis of Advanced High Voltage Direct Current Transmission Systems","authors":"Ghulam Muhay Ud Din, Nusrat Husain, Ashraf Yahya, Z. Arfeen","doi":"10.1109/ICAEM53552.2021.9547195","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547195","url":null,"abstract":"The transmission of power with the help of high voltage alternating current (HVAC) is a conventional technique. On the other hand, transferring huge power over extensive distances using high voltage direct current (HVDC) systems is a developing and advanced technique. Although from 1950, researchers and technologists have achieved significant development in HVDC transmission systems that were based on mercury-arc valves, an important milestone was completed in the 1970s, when the thyristors switching technologies were adopted in the line commutated converter (LCC) based HVDC power transmissions. Since 1997, the evolution of power transistor-based voltage source converter (VSC) technology, and then in 2010, the modular multilevel converter (MMC) technology, opened new eras in the advanced HVDC transmission systems. With the help of pulse width modulation (PWM) based VSC, and MMC technologies, the field operators can control the real and imaginary powers, individualistically. The short length asynchronous interconnections can also be possible with these technologies. This paper will discuss the mathematical analysis of advanced HVDC transmission systems, having tie lines and power converters, and HVDC transmission for bulk solar photovoltaic (PV) power generation.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"188 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116603275","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
A. Rehman, Misha Urooj Khan, Muhammad Zulqarnain Haider Ali, M. S. Shah, M. F. Ullah, Mehwish Ayub
{"title":"Stability Enhancement of Commercial Boeing Aircraft with Integration of PID Controller","authors":"A. Rehman, Misha Urooj Khan, Muhammad Zulqarnain Haider Ali, M. S. Shah, M. F. Ullah, Mehwish Ayub","doi":"10.1109/ICAEM53552.2021.9547186","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547186","url":null,"abstract":"It is critical in aircraft design to analyze the behavior, effectiveness, reliability, and other elements of the systems prior to commercial deployment. To design a stable aviation control system, a strong mathematical model of the system is required so that its behavior can be clearly comprehended and regulated. The state-space model of an autopiloted airplane is developed in this article utilizing MATLAB because this simulation model will help gather knowledge in order to make judgments at all phases of airplane development. We focused solely on stability, emphasizing the system's rapid settling without substantial overshoots. The MATLAB state-space model is effectively developed and simulated with and without a controller. The aircraft angle, pitch rate, and pitch angle are chosen as state variables. With the help of the PID controller, we achieved a settling time of 0.0741s and a rise time of 0.0390s.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124909442","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Misha Urooj Khan, Sana Samer, Aqsa Samer, Areeba Mobeen, A. Arshad, Hareem Khan
{"title":"Classification of Phonocardiography based Heart Auscultations while Listening to Tilawat-e-Quran and Music Using Vibrational Mode Decomposition","authors":"Misha Urooj Khan, Sana Samer, Aqsa Samer, Areeba Mobeen, A. Arshad, Hareem Khan","doi":"10.1109/ICAEM53552.2021.9547150","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547150","url":null,"abstract":"Tension and depression are emotional feelings caused by tough life routines and situations. People are under stress due to their work, daily problems, and loss in their business. So, they use many channels and mediums to release this stress. One of the most frequently used methods is listening to music and their Holy scripts. Muslims strongly believe that their Holy book Al-Quran is the firmest way of bringing peace and pleasure in their life. Its recitation helps people relax and release the pain of patients having mental and physical sickness. To prove this scientifically, researchers evaluate the effect on the heart and brain during Holy Quran's recitation and listening. In this paper, our main focus is to analyze the activity of the heart. We are using Phonocardiogram (PCG) based heart auscultations to test the heartbeat rate before and after listening to the Holy Quran and music. PCG signals are collected from 47 subjects during three conditions, i.e., during normal, Quran, and music listening. With the help of pre-processing, segmentation, and Neural network techniques, we achieved a cumulative accuracy of 98.6%. Thus, it proves the fact that Tilawat-e-Quran brings calmness and happiness to the heart as compared to music listening.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"78 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124544346","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Life Prediction of a Scaled Down Fabricated Tracked Vehicle Model","authors":"Ayaz M. Khan, Shahid Khalil, Y. Hamid","doi":"10.1109/ICAEM53552.2021.9547135","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547135","url":null,"abstract":"Tracked vehicles are meant to traverse through different ground conditions such as plane road, undulated terrain, marshy areas, etc. due to which the track is subjected to different loading conditions that causes failures in track with time. The track link testing procedure takes about 1–2 years in selecting, testing and finalizing the track sample. To reduce the involved time, effort and cost, this work would focus on fabrication of a lab-based setup so as to reduce the experimental procedure time in accordance to existing Acceptance testing procedure (ATP). According to best of the authors knowledge there is no such existing setup for testing a track link. The work would focus on design and fabrication of a scale down model based on the mean maximum pressure (MMP). The setup is then used to predict life of track link using stress-life approach which was about 8000 cycles.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"182 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124586332","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Classification of Diseases in Citrus Fruits using SqueezeNet","authors":"E. Khan, M. F. U. Rehman, Fawad Ahmed, M. A. Khan","doi":"10.1109/ICAEM53552.2021.9547133","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547133","url":null,"abstract":"Recent advances in AI technology have paved the way to precisely detect and classify fruit and vegetable diseases. Vision based accurate detection and classification techniques can help farmers to quickly identify different types of plant and fruit diseases. Citrus fruits are globally famous due to their taste and nutrients. In this paper, a deep learning-based technique is proposed for classification of six different citrus diseases that severely affect the yield and quality of citrus fruits. Data augmentation is performed to enlarge the privately acquired dataset. Later the augmented dataset is used to retrain two lightweight pre-trained deep learning models; the SqueezeNet and MobileNetV2. Features are extracted from the retrained models which are subsequently optimized by using the Whale Optimization Algorithm. Classification results obtained from both the models show that the SqueezeNet model outperforms MobileNetV2 and attains an accuracy of 96%. The proposed citrus fruit disease classification technique also outperforms when compared with a current technique proposed in the literature","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"5 2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123634176","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Modified Residual Power Series Method for Boundary Value Problems","authors":"Mubashir Qayyum, Qursam Fatima","doi":"10.1109/ICAEM53552.2021.9547092","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547092","url":null,"abstract":"In this manuscript, a new modification of residual power series method (RPSM) has been introduced for the solution of ordinary differential equations (ODEs) with boundary conditions. Proposed scheme has been applied to linear and nonlinear test problems of order two and four. Comparison of the obtained results are made with optimal varitional iterational method (OVIM) and modified variation iteration method (MVIM) to confirm the efficiency and reliability of the proposed scheme. Analysis reveals that RPSM is effective and efficient way to tackle a wide variety of BVPs.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129374410","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Brain Tumor Segmentation and Classification using Machine Learning","authors":"Hassan Habib, Awais Mehmood, Tahira Nazir, M. Nawaz, Momina Masood, Rabbia Mahum","doi":"10.1109/ICAEM53552.2021.9547084","DOIUrl":"https://doi.org/10.1109/ICAEM53552.2021.9547084","url":null,"abstract":"Brain Tumor segmentation and classification is an interesting yet challenging research domain of Biomedical Image processing. So, extracting useful information, segment an image correctly, classify an image, and accurately predict the result, not an easy task. For better segmentation and classification of any bio-medical image processing, we must focus on a good dataset, a better understanding of statistics, and better algorithms for processing image datasets. This research focuses on accurately classify tumors from MRI images using multiple Segmentation algorithms to overcome the slight chance of miss classification Error. Multiple segmentation algorithms help to generate more accurate and precise results as compared to a single segmentation algorithm. For this purpose, watershed, K-means, and Threshold segmentation algorithm are used along with SVM Classifier and finally achieve 90% above classification result at the end.","PeriodicalId":219957,"journal":{"name":"2021 International Conference on Applied and Engineering Mathematics (ICAEM)","volume":"89 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-08-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127585359","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}