فهرس المقالات Propeller

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  1 - Qualification of Propeller by Experimental and Analytical Methods
  K. Siva Prasad S. Murthy Bellala
  The paper focuses on static and dynamic analysis of propeller blade made of Aluminium-24345 material. The solid model of propeller blade and propeller are developed in CATIA V5 R20. By using this model, propeller blade was manufactured using 3-Axis CNC milling machine b أکثر

  The paper focuses on static and dynamic analysis of propeller blade made of Aluminium-24345 material. The solid model of propeller blade and propeller are developed in CATIA V5 R20. By using this model, propeller blade was manufactured using 3-Axis CNC milling machine by adopting MASTERCAM software. Qualification tests were carried out on the propeller blade of an underwater vehicle for their strength and vibration. Impact Hammer Method is employed to measure the vibration-damping properties of Propeller blade. Computational Fluid Dynamics (CFD) analysis is carried out to analyze the contours of static pressure on the 5-Blade propeller and the forces, moments acting on the propeller. Finite element analysis (FEA) of the blade was carried in ANSYS 15.0. Static, modal, harmonic analysis was carried out on analysis software for the modeled propeller blade and Factor of Safety was determined to qualify the propeller.Deformation of the propeller blade is measured using Coordinate Measuring Machine (CMM). تفاصيل المقالة
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  2 - A Simple Method for Designing a Duct for a Multi-Component Ducted Propulsion System
  N. M. Nouri Mehrdad Kalantar Neyestanaki Saber Mohammadi
  The present paper numerically discusses the design procedure of marine ducts used for multi-component ducted propulsion systems at the stern of an axisymmetric submerged body. The results are presented in the form of tables showing the effects of dihedral angel as well أکثر

  The present paper numerically discusses the design procedure of marine ducts used for multi-component ducted propulsion systems at the stern of an axisymmetric submerged body. The results are presented in the form of tables showing the effects of dihedral angel as well as camber ratio of the duct as the two most important geometrical parameters on hydrodynamic performance of the propulsion system. Furthermore, a correlation has been extracted between the results of two and three dimensional analysis of ducted propellers. The results show that the design procedure of the duct used for a ducted propulsion system could be performed using some two dimensional analyses. The simulations are performed using a Reynolds averaged Navier Stokes Equations (RANS) based Computational Fluid Dynamics (CFD) tool. تفاصيل المقالة
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  3 - A Quasi-Analytical Method Algorithm Development in Redesigning the Geometry and Structural Analysis of An Aircraft Propeller and Comparing with the Finite Element Method
  Behrooz Shahriari Hassan Izanlo Nedasadat  Seddighi
  The aircraft propeller is effective in the performance of the aircraft propulsion system and must have acceptable structural strength. The complex aerodynamic geometry of the propeller makes its analysis more difficult. In this study, dynamic and aerodynamic stresses ar أکثر

  The aircraft propeller is effective in the performance of the aircraft propulsion system and must have acceptable structural strength. The complex aerodynamic geometry of the propeller makes its analysis more difficult. In this study, dynamic and aerodynamic stresses are calculated using the Finite Element Method (FEM). A structural analysis algorithm based on the quasi-analytical method is developed to evaluate the finite element analysis. In this regard, first, an algorithm is developed to redesign the propeller which performs in a way that by checking the dimensions, the geometry of the quasi-propeller is determined with the same mass and the coordinates of the center of mass. Then, different algorithms are developed to calculate the distribution of mass, moment of inertia, and the cross-section of the quasi-blade geometry. The calculation algorithms of rotational dynamic and aerodynamic stress distribution are developed. The results show that the FEM and the quasi-analytical method are well matched. In this study, the force equivalent to the thrust and the opposite force to the propeller rotation are placed instead of the aerodynamic pressure distribution. The comparison of the results obtained from the quasi-analytical method and the FEM indicates that the overall maximum stress of the system occurs at the root of the propeller and the maximum net stress due to aerodynamic forces occurs in the middle of the propeller geometry. According to the results, the rotational dynamic stress is much higher than the aerodynamic stress. It is also shown that the aerodynamic stress reduces the overall stress of the system. تفاصيل المقالة
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  4 - بررسی ارتعاشات سازه شناور در اثر تحریک پروانه با استفاده از تحلیل عددی سیال-سازه (FSI)
  مهدیه سادات عزیزی یوسف امیریان عبدالحسین فریدون
  ارتعاشات سازه شناور در اثر تحریک پروانه، یکی از مباحث مهم در طراحی سازه شناور است. در صورت عدم توجه به این مساله و قرار‌گیری سوپراستراکچر در قسمت انتهایی شناور، ارتعاشات ناشی از تحریک پروانه می تواند مشکلاتی را برای خدمه و افراد ایجاد نماید. همچنین ارتعاشات ناشی از پروا أکثر

  ارتعاشات سازه شناور در اثر تحریک پروانه، یکی از مباحث مهم در طراحی سازه شناور است. در صورت عدم توجه به این مساله و قرار‌گیری سوپراستراکچر در قسمت انتهایی شناور، ارتعاشات ناشی از تحریک پروانه می تواند مشکلاتی را برای خدمه و افراد ایجاد نماید. همچنین ارتعاشات ناشی از پروانه باعث سر و صدا و همچنین کاهش عمر ماشین آلات موجود در موتورخانه و قسمت انتهایی شناور می‌گردد. در این مقاله ارتعاشات ناشی از تحریک پروانه، با استفاده از تحلیل عددی سیال- سازه روی یک شناور تجاری مورد بررسی قرار گرفته و به بررسی نتایج آن پرداخته شده است. ابتدا برای شناور با توجه به هندسه و شرایط، پروانه ای مناسب انتخاب شده و حل عددی جریان سیال برای سرعت های مختلف شناور و سرعت دورانی پروانه انجام گرفته است. سپس سازه شناور بر اساس استاندارد، طراحی شده و جز‌بندی آن با استفاده از جزء محدود صفحه ای انجام گرفته است. توزیع فشار روی پروانه و بدنه که از حل عددی جریان سیال به دست آمده است در تحلیل سازه، به سازه شناور اعمال گشته و سازه شناور در اثر بارگذاری هارمونیک ناشی از دوران پروانه، بررسی شده است. تحلیل مودال سازه شناور نیز انجام گرفته و سپس نتایج تحلیل آن، در یک محدوده فرکانسی شامل فرکانس های طبیعی که می تواند در حالت ها و سرعت های مختلف دورانی پروانه به وجود آید، استخراج شده است. نتایج نشان می دهد که در بعضی از سرعت های دورانی پروانه، فرکانس تحریک در سرعت دورانی مربوطه می تواند منجر به تشدید ارتعاش و افزایش دامنه ی ارتعاش گردد. نتایج با محدوده مجاز استاندارد مقایسه شده و نشان می دهد که می توان با دقت در انتخاب پروانه و محدوده سرعت دورانی مجاز و بهینه سازی و اصلاح سازه شرایط را جهت قرارگیری ارتعاشات در محدوده ی مجاز فراهم نمود. تفاصيل المقالة
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  5 - Numerical solution of hovering propeller performance at various blade pitch angles and revolutions with different turbulence models
  Behrooz Shahriari Mohammad Reza Hashemi
  In this research the validation of different turbulence models of a hovering propeller at different pitch angles and revolutions has been investigated. For this purpose, the pressure on the propeller surface at different cross sections has been calculated numerically by أکثر

  In this research the validation of different turbulence models of a hovering propeller at different pitch angles and revolutions has been investigated. For this purpose, the pressure on the propeller surface at different cross sections has been calculated numerically by six different turbulence models and compared with the experimental data. In the first part, the effects of changing the blade angle have been discussed, in this case, the angles of 0, 2, and 12 degrees have been selected. The results showed that changes in the pitch angle of the propeller have led to an increase in the error rate of numerical calculations. At a high pitch angle and in the same chord section, the highest amount of error is produced in leading edge section of the propeller, among which the best model in terms of production error is the k-e RNG. Also, due to the possibility of the formation of shock waves, the S-A and k-e standard models have very large errors, which shows these models' inability to simulate rotating flow with shock waves. تفاصيل المقالة