This certificate of participation certifies that Abhijeet Sunil Gaikwad from AISSMS College of Engineering participated in the SAE Aero Design West competition held from April 22, 2016 to April 24, 2016 in Van Nuys, California, United States.
This certificate of participation recognizes Ali Adel Salem of Alexandria University for participating in the SAE Aero Design East competition held from March 11-13, 2016 in Fort Worth, Texas. The certificate confirms Ali Adel Salem's involvement in the competition organized by the Society of Automotive Engineers.
This certificate was presented to Arnab Raychaudhari on June 1, 2018 for successfully completing the Pre-Sales SAM Specialization course. The certificate was generated from a ServiceNow instance and includes a link to view the full certificate details.
Rei Sivan completed the HDE 110 - MapR Distribution Essentials course offered by MapR Academy on August 15, 2015. A certificate of completion was issued with certificate number 9d5dv845nu6y, which can be verified online at http://verify.skilljar.com/c/9d5dv845nu6y.
This certificate was presented to Arnab Raychaudhari on June 1, 2018 for successfully completing the Pre-Sales PA Specialization course. The certificate was issued through the ServiceNow Saba Cloud production environment and linked to a specific certificate template and learner record.
This certificate from Google awards Jaiser Abbas certification in AdWords Mobile Advertising by passing the AdWords Fundamentals and Mobile Advertising exams. The certificate is valid until October 20, 2017 according to the document issued by Google Partners.
This document is a thank you page from McAfee for downloading a free trial of their antivirus software. It confirms the download and prompts the user to install and run the software to start protecting their device. Instructions are provided on registering for the full version once the trial expires.
Asif Sharafudeen is seeking a challenging career in the maritime industry. He has a B.Tech in Marine Engineering and 8 months of pre-sea training experience. His skills include maintenance of marine diesel engines and auxiliary machines, knowledge of firefighting equipment, pumps, motors and alternators used on board vessels. He is proficient in survival techniques, first aid, and has security training. Currently he works as a crane mechanic in Dubai.
The document discusses reaching the right audience by integrating audience targeting with apps. It provides information on modularity, extensibility, integrability and an API for accessing services at http://localhost:8080/api/jsonws. It directs the reader to more information and tutorials on developing with Liferay on dev.liferay.com and encourages providing feedback by rating the session in a mobile app.
This certificate of participation recognizes Ali Adel Salem of Alexandria University for participating in the SAE Aero Design East competition held from March 11-13, 2016 in Fort Worth, Texas. The certificate confirms Ali Adel Salem's involvement in the competition organized by the Society of Automotive Engineers.
This certificate was presented to Arnab Raychaudhari on June 1, 2018 for successfully completing the Pre-Sales SAM Specialization course. The certificate was generated from a ServiceNow instance and includes a link to view the full certificate details.
Rei Sivan completed the HDE 110 - MapR Distribution Essentials course offered by MapR Academy on August 15, 2015. A certificate of completion was issued with certificate number 9d5dv845nu6y, which can be verified online at http://verify.skilljar.com/c/9d5dv845nu6y.
This certificate was presented to Arnab Raychaudhari on June 1, 2018 for successfully completing the Pre-Sales PA Specialization course. The certificate was issued through the ServiceNow Saba Cloud production environment and linked to a specific certificate template and learner record.
This certificate from Google awards Jaiser Abbas certification in AdWords Mobile Advertising by passing the AdWords Fundamentals and Mobile Advertising exams. The certificate is valid until October 20, 2017 according to the document issued by Google Partners.
This document is a thank you page from McAfee for downloading a free trial of their antivirus software. It confirms the download and prompts the user to install and run the software to start protecting their device. Instructions are provided on registering for the full version once the trial expires.
Asif Sharafudeen is seeking a challenging career in the maritime industry. He has a B.Tech in Marine Engineering and 8 months of pre-sea training experience. His skills include maintenance of marine diesel engines and auxiliary machines, knowledge of firefighting equipment, pumps, motors and alternators used on board vessels. He is proficient in survival techniques, first aid, and has security training. Currently he works as a crane mechanic in Dubai.
The document discusses reaching the right audience by integrating audience targeting with apps. It provides information on modularity, extensibility, integrability and an API for accessing services at http://localhost:8080/api/jsonws. It directs the reader to more information and tutorials on developing with Liferay on dev.liferay.com and encourages providing feedback by rating the session in a mobile app.
This document provides instructions for designing a paper aircraft in 12 steps. The steps include folding a sheet of paper in half lengthwise to create a center fold guideline, then making a series of folds along the guideline and specified dimensions to form the fuselage, wings and fins. The final steps involve folding down the wings and fins and calibrating the aircraft before its inaugural flight. Following the instructions should enable students to design their own paper aircraft by the end of the lesson.
1) The document describes a design for improving the preventative maintenance program at Amgen to increase efficiency and effectiveness.
2) Key aspects of the new design include removing redundant or unnecessary tasks, optimizing task frequencies, adding new tasks based on failure history, and training operators to perform some tasks to reduce maintenance costs and downtime.
3) For the improvements to be sustainable, the updated preventative maintenance program needs to be fully implemented and continuous improvement processes established.
Selection and analysis of the landing gear for unmanned aerial vehicle for sa...IAEME Publication
The document discusses the selection and analysis of a landing gear design for an unmanned aerial vehicle to compete in the SAE Aero Design Series competition. It describes different types of landing gear configurations, including tail wheel, tandem, and tricycle types. It then details the selection of a tricycle-type landing gear for the specific unmanned aerial vehicle due to its ease of ground operations. A finite element analysis was performed on the selected landing gear design to analyze deformation and stresses under expected landing impact forces, with the results showing a factor of safety above 2, indicating a safe design.
The document provides information about rule changes for the 2016 SAE Aero Design competition, including new requirements for the Advanced Class. Major changes include allowing multiple payload drops per flight in Advanced Class, which will significantly impact aircraft center of gravity. Advanced Class aircraft must now prove they can successfully fly, drop a payload, and land before competing. The rules format has been rewritten for easier reading. Teams are advised to carefully read and understand all rules changes, as missing a change could prevent them from competing.
The document discusses the SAEINDIA National Student Convention 2010. It provides details on the objectives and format of the convention, including contests and sponsorship opportunities. Previous conventions are summarized, noting growing participation from colleges and students. The convention aims to showcase student capabilities, share experiences, and motivate involvement in automotive sciences. It provides opportunities for students, colleges, divisions, members, sponsors.
The Polytechnic University of Puerto Rico's SAE Aero Design team is seeking sponsorship to participate in the 2015 SAE Aero Design West competition in California. The team will design and build a remote-controlled aircraft for the micro class competition, which requires carrying the maximum payload weight with the lowest empty aircraft weight. The sponsorship package outlines different sponsorship levels and benefits, with funds going towards materials, manufacturing, registration fees, and travel costs for the 11 student team members. The team's goal is to gain hands-on engineering experience and represent their university at the national competition.
The document is a sponsorship proposal from the SAE Aero Design team of Polytechnic University of Puerto Rico. The team is seeking sponsorship to design and build a remote controlled aircraft to compete in the SAE Aero Design competition in order to apply their engineering knowledge and skills. The competition involves designing planes that can lift the most payload weight. The proposal provides details on the competition categories, the team members, and sponsorship packages available to support the team's participation.
This document provides a design report for an aircraft competing in the Micro Class category of the SAE Aero Design competition. Key aspects of the design include selecting lightweight materials like balsa wood and carbon fiber to achieve a high payload fraction of around 90%. Analytical tools like Creo and Excel were used to simulate and optimize the design. A straight high wing configuration with a NACA S1223 airfoil was chosen. Performance analysis determined the aircraft needs a launch speed of around 35 mph and can fly between 40-55 mph powered by an 11" diameter propeller. The design was optimized to meet competition requirements while achieving the team's goals.
The document describes a conceptual design for a take-off and landing system (TLS) for the Insitu Integrator unmanned aircraft system. It provides background details on the aircraft configuration, structural scheme, and current TLS. Five concepts for a new TLS were generated and two were selected for further analysis based on a trade study. The feasibility of integrating the selected concepts with the aircraft was then evaluated through analytical calculations and simulations. A failure modes and effects analysis was also conducted to assess the safety of the proposed design. The results were discussed to evaluate the feasibility and suitability of the new TLS concept for the Integrator.
Do you look for a guide about how to build a rc plane? We are focusing parkjet designs, here is a guide that you can learn to build a parkjet. Check out http://onlinereview101.blogspot.com/2014/12/how-to-make-rc-airplane.html
Basic Info regarding making a RC aeroplaneZubair Ahmed
The document provides information on the control surfaces and aerodynamic components of an aircraft. It discusses that elevators control pitch, ailerons control roll, and the rudder controls yaw. It also mentions vertical and horizontal stabilizers provide stability and prevent pitching and yawing motions. The document further provides details on requirements, wing design and construction, airfoils, servos, engines, batteries, and tips for stability.
Introduction to Radio Controlled PlanesMostafa Eid
This is an introductory for beginners who do not know where to start or how to start, so this comprehensive session states the major types of RC Aircrafts which shall allow you to search deeply in one or all of these categories
O documento discute os principais componentes de uma aeronave, incluindo:
1) Estrutura da aeronave, asas, empenagem e estabilizadores;
2) Sistemas de controle de voo e superfícies móveis;
3) Motores e sistemas de propulsão.
This document outlines a project to design a radio controlled model airplane to set a new FAI world endurance record for electric powered airplanes. The key objectives are to exceed the current record of 12 hours and 36 minutes while meeting FAI requirements. The document discusses the physics challenges, potential design approaches for the airplane and propulsion systems, and the importance of design trade studies and testing to optimize endurance. It provides initial estimates for wing area, aspect ratio, weight distribution and performance predictions to guide the design process.
This document summarizes the design of a remote controlled aircraft. It discusses selecting a symmetrical airfoil with a NACA0012 profile for its low speed stability. It describes control surfaces like ailerons and elevators. Calculations are shown for wing area based on lift and drag coefficients. A CATIA model and flow simulation were also created. The design focuses on stability concepts like neutral point, center of pressure, and aerodynamic center. References include aerodynamics textbooks and software used like JAVA, Flow Design, and CATIA V5.
The document outlines the plans for the SAE Aero design team from Kjsce that will be competing in an annual international aerospace design competition held in Forth Worth, Texas each March. The team consists of subgroups focused on structural design, aerodynamics, materials management, and marketing/publicity. The team needs a workshop space of at least 200 square feet with a computer, various tools for one-time investment, and recurring expenses including an engine, balsa wood, transmitter radio, and batteries that total around Rs. 51,000.
This presentation discusses swept wing configurations and their applications for supersonic flight. Swept wings reduce wave drag at transonic speeds by angling shock waves away from the aircraft. Swept wings were first developed in Germany in the 1930s and became prominent with aircraft like the MiG-15 and F-86. Variations include forward swept wings, which provide maneuverability but are expensive, and variable sweep wings which can change sweep angle during flight. Swept wings provide benefits like lateral stability and delaying compressibility effects at transonic speeds.
The document is a design report for an aircraft called the L-406 Skycrane that was designed to compete in the Micro Class of the 2015 SAE Aero Design West competition. Some key points:
1) The aircraft was designed to have a maximum weight of 10 pounds and fit within a 6-inch diameter container in order to comply with competition rules. The goal was to achieve a high payload fraction of approximately 80%.
2) An innovative aspect of the design was that the entire aircraft was manufactured using additive manufacturing to reduce weight and accelerate the production process.
3) Performance analyses were conducted to determine that the aircraft could be hand-launched at 30 feet per second, complete two 180-degree
The document provides a preliminary design for a regional passenger aircraft. It discusses the main components needed for the design, including the wing, fuselage, and empennage. For the wing, 18 key parameters are identified that must be determined, such as wing area, aspect ratio, and airfoil shape. The fuselage is designed to house passengers and cargo while withstanding cabin pressure. Key empennage parameters that require determination include the horizontal and vertical tail sizes, sweeps, and chords. The document outlines the initial steps in conceptualizing and designing a new regional aircraft.
This document summarizes different types of airplane wings. It describes straight wings, swept-back wings, delta wings, forward-swept wings, variable-sweep wings, flying wings, dihedral wings, tapered wings, and variable geometry wings. For each type, it provides a brief definition and example shape. The document aims to provide an overview of the various wing designs used in aircraft.
This document provides instructions for designing a paper aircraft in 12 steps. The steps include folding a sheet of paper in half lengthwise to create a center fold guideline, then making a series of folds along the guideline and specified dimensions to form the fuselage, wings and fins. The final steps involve folding down the wings and fins and calibrating the aircraft before its inaugural flight. Following the instructions should enable students to design their own paper aircraft by the end of the lesson.
1) The document describes a design for improving the preventative maintenance program at Amgen to increase efficiency and effectiveness.
2) Key aspects of the new design include removing redundant or unnecessary tasks, optimizing task frequencies, adding new tasks based on failure history, and training operators to perform some tasks to reduce maintenance costs and downtime.
3) For the improvements to be sustainable, the updated preventative maintenance program needs to be fully implemented and continuous improvement processes established.
Selection and analysis of the landing gear for unmanned aerial vehicle for sa...IAEME Publication
The document discusses the selection and analysis of a landing gear design for an unmanned aerial vehicle to compete in the SAE Aero Design Series competition. It describes different types of landing gear configurations, including tail wheel, tandem, and tricycle types. It then details the selection of a tricycle-type landing gear for the specific unmanned aerial vehicle due to its ease of ground operations. A finite element analysis was performed on the selected landing gear design to analyze deformation and stresses under expected landing impact forces, with the results showing a factor of safety above 2, indicating a safe design.
The document provides information about rule changes for the 2016 SAE Aero Design competition, including new requirements for the Advanced Class. Major changes include allowing multiple payload drops per flight in Advanced Class, which will significantly impact aircraft center of gravity. Advanced Class aircraft must now prove they can successfully fly, drop a payload, and land before competing. The rules format has been rewritten for easier reading. Teams are advised to carefully read and understand all rules changes, as missing a change could prevent them from competing.
The document discusses the SAEINDIA National Student Convention 2010. It provides details on the objectives and format of the convention, including contests and sponsorship opportunities. Previous conventions are summarized, noting growing participation from colleges and students. The convention aims to showcase student capabilities, share experiences, and motivate involvement in automotive sciences. It provides opportunities for students, colleges, divisions, members, sponsors.
The Polytechnic University of Puerto Rico's SAE Aero Design team is seeking sponsorship to participate in the 2015 SAE Aero Design West competition in California. The team will design and build a remote-controlled aircraft for the micro class competition, which requires carrying the maximum payload weight with the lowest empty aircraft weight. The sponsorship package outlines different sponsorship levels and benefits, with funds going towards materials, manufacturing, registration fees, and travel costs for the 11 student team members. The team's goal is to gain hands-on engineering experience and represent their university at the national competition.
The document is a sponsorship proposal from the SAE Aero Design team of Polytechnic University of Puerto Rico. The team is seeking sponsorship to design and build a remote controlled aircraft to compete in the SAE Aero Design competition in order to apply their engineering knowledge and skills. The competition involves designing planes that can lift the most payload weight. The proposal provides details on the competition categories, the team members, and sponsorship packages available to support the team's participation.
This document provides a design report for an aircraft competing in the Micro Class category of the SAE Aero Design competition. Key aspects of the design include selecting lightweight materials like balsa wood and carbon fiber to achieve a high payload fraction of around 90%. Analytical tools like Creo and Excel were used to simulate and optimize the design. A straight high wing configuration with a NACA S1223 airfoil was chosen. Performance analysis determined the aircraft needs a launch speed of around 35 mph and can fly between 40-55 mph powered by an 11" diameter propeller. The design was optimized to meet competition requirements while achieving the team's goals.
The document describes a conceptual design for a take-off and landing system (TLS) for the Insitu Integrator unmanned aircraft system. It provides background details on the aircraft configuration, structural scheme, and current TLS. Five concepts for a new TLS were generated and two were selected for further analysis based on a trade study. The feasibility of integrating the selected concepts with the aircraft was then evaluated through analytical calculations and simulations. A failure modes and effects analysis was also conducted to assess the safety of the proposed design. The results were discussed to evaluate the feasibility and suitability of the new TLS concept for the Integrator.
Do you look for a guide about how to build a rc plane? We are focusing parkjet designs, here is a guide that you can learn to build a parkjet. Check out http://onlinereview101.blogspot.com/2014/12/how-to-make-rc-airplane.html
Basic Info regarding making a RC aeroplaneZubair Ahmed
The document provides information on the control surfaces and aerodynamic components of an aircraft. It discusses that elevators control pitch, ailerons control roll, and the rudder controls yaw. It also mentions vertical and horizontal stabilizers provide stability and prevent pitching and yawing motions. The document further provides details on requirements, wing design and construction, airfoils, servos, engines, batteries, and tips for stability.
Introduction to Radio Controlled PlanesMostafa Eid
This is an introductory for beginners who do not know where to start or how to start, so this comprehensive session states the major types of RC Aircrafts which shall allow you to search deeply in one or all of these categories
O documento discute os principais componentes de uma aeronave, incluindo:
1) Estrutura da aeronave, asas, empenagem e estabilizadores;
2) Sistemas de controle de voo e superfícies móveis;
3) Motores e sistemas de propulsão.
This document outlines a project to design a radio controlled model airplane to set a new FAI world endurance record for electric powered airplanes. The key objectives are to exceed the current record of 12 hours and 36 minutes while meeting FAI requirements. The document discusses the physics challenges, potential design approaches for the airplane and propulsion systems, and the importance of design trade studies and testing to optimize endurance. It provides initial estimates for wing area, aspect ratio, weight distribution and performance predictions to guide the design process.
This document summarizes the design of a remote controlled aircraft. It discusses selecting a symmetrical airfoil with a NACA0012 profile for its low speed stability. It describes control surfaces like ailerons and elevators. Calculations are shown for wing area based on lift and drag coefficients. A CATIA model and flow simulation were also created. The design focuses on stability concepts like neutral point, center of pressure, and aerodynamic center. References include aerodynamics textbooks and software used like JAVA, Flow Design, and CATIA V5.
The document outlines the plans for the SAE Aero design team from Kjsce that will be competing in an annual international aerospace design competition held in Forth Worth, Texas each March. The team consists of subgroups focused on structural design, aerodynamics, materials management, and marketing/publicity. The team needs a workshop space of at least 200 square feet with a computer, various tools for one-time investment, and recurring expenses including an engine, balsa wood, transmitter radio, and batteries that total around Rs. 51,000.
This presentation discusses swept wing configurations and their applications for supersonic flight. Swept wings reduce wave drag at transonic speeds by angling shock waves away from the aircraft. Swept wings were first developed in Germany in the 1930s and became prominent with aircraft like the MiG-15 and F-86. Variations include forward swept wings, which provide maneuverability but are expensive, and variable sweep wings which can change sweep angle during flight. Swept wings provide benefits like lateral stability and delaying compressibility effects at transonic speeds.
The document is a design report for an aircraft called the L-406 Skycrane that was designed to compete in the Micro Class of the 2015 SAE Aero Design West competition. Some key points:
1) The aircraft was designed to have a maximum weight of 10 pounds and fit within a 6-inch diameter container in order to comply with competition rules. The goal was to achieve a high payload fraction of approximately 80%.
2) An innovative aspect of the design was that the entire aircraft was manufactured using additive manufacturing to reduce weight and accelerate the production process.
3) Performance analyses were conducted to determine that the aircraft could be hand-launched at 30 feet per second, complete two 180-degree
The document provides a preliminary design for a regional passenger aircraft. It discusses the main components needed for the design, including the wing, fuselage, and empennage. For the wing, 18 key parameters are identified that must be determined, such as wing area, aspect ratio, and airfoil shape. The fuselage is designed to house passengers and cargo while withstanding cabin pressure. Key empennage parameters that require determination include the horizontal and vertical tail sizes, sweeps, and chords. The document outlines the initial steps in conceptualizing and designing a new regional aircraft.
This document summarizes different types of airplane wings. It describes straight wings, swept-back wings, delta wings, forward-swept wings, variable-sweep wings, flying wings, dihedral wings, tapered wings, and variable geometry wings. For each type, it provides a brief definition and example shape. The document aims to provide an overview of the various wing designs used in aircraft.