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Sensors VS Transducers
This document discusses various sensors and transducers. It defines a transducer as a device that converts one form of energy to another, and a sensor as a transducer that detects a characteristic of its environment. It then provides details on different types of transducers and sensors, including antennas, Hall effect sensors, cathode ray tubes, sensors for ionizing radiation, electric current sensors, and proximity sensors. For each it discusses their definition, operating principle, applications and examples. The document is authored by several students and provides a comprehensive overview of key sensors and transducers.
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Aircraft turbine blades and expected advancement in technology using carbon n...
Gas turbines are of prime importance to aircrafts. The turbo machinery is a complex aspect of designing. Efficiency of turbo machinery is closely proportional to material selection and its performance. Each section of a turbo machinery deserves or has a different criteria of temperature dependency. As per this dependency turbine blades, nozzles and wheels are designed using different types of materials- alloys, which are highly resistant to temperature and light weight. This will lead to aircrafts which are very light and highly efficient. These materials are alloys which are very costly. And this high cost are making them difficult to be used abundantly. All these problems has made researchers to look around for material which is light, comparatively cheap and highly efficient as per turbine needs. This paper throws light on the existing materials used in turbine blades and a new compound which is a carbon allotrope which is capable of meeting all above needs perfectly.
Jean-Paul Gibson: Aerolab Subsonic Wind Tunnel Report
In this lab data was collected from (18) separate tap points along an airfoil within a subsonic wind tunnel generating winds at 70 miles per hour. In addition, this data was gathered for (4) different angles of attack.
The purpose of this lab was to calculate the pressure coefficient at each of those tap points. Our calculated results for the lab were compared to that of a manual that was provided for this experiment.
Recommended
Catapult Into History
The document summarizes the history and evolution of catapult technology from ancient times. It describes how early tension catapults used bending wood or animal horns as power sources, while later torsion catapults relied on tightly coiled ropes to hurl projectiles. Traction trebuchets introduced levers for quick operation and accuracy. The most advanced gravity trebuchets generated power from very heavy falling weights to launch projectiles over even greater distances.
Catapult Crossfire
This document summarizes a student project to design and build a functioning catapult prototype called Catapult Crossfire. It involved applying the design techniques learned in their ME 371 lecture course. Several methods were used in the design process, including hand sketches, calculations, and CAD software. NX CAD specifically aided in determining linkage angles and optimizing the design. The project also required selecting appropriate materials and using tools like a lathe, mill, and drill press to construct the physical prototype. Key components of the design included a four-bar linkage, overdrive gear setup, and cam mechanism. Equations from the lecture course informed the theoretical design.
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This document discusses the effects of high speeds on tire couplings. It explains that as speed increases, centrifugal force causes the elastomeric tire element to expand radially and compress axially. This axial compression increases thrust forces on attached equipment and reduces equipment life. It also notes that high speeds can cause resonance vibrations that damage the coupling over time. The document analyzes how the distance between coupling flanges decreases with increasing speed due to radial expansion of the tire. It concludes that compensating for deformation through flange spacing adjustment and reinforcing the tire toe with a bead can help address issues caused by high speed centrifugal forces and vibrations.
Sensors VS Transducers
This document discusses various sensors and transducers. It defines a transducer as a device that converts one form of energy to another, and a sensor as a transducer that detects a characteristic of its environment. It then provides details on different types of transducers and sensors, including antennas, Hall effect sensors, cathode ray tubes, sensors for ionizing radiation, electric current sensors, and proximity sensors. For each it discusses their definition, operating principle, applications and examples. The document is authored by several students and provides a comprehensive overview of key sensors and transducers.
Sensors presentation-06a
The document discusses sensors and their use in museums. It begins by defining sensors as miniature devices that capture sensory data like heat, light, and humidity in response to external stimuli. It then outlines how sensors could enhance museum experiences by enabling ubiquitous computing, planned activities, and new interactive paradigms. The rest of the document details sensor frameworks, various sensor types, their properties, and how they could transform user experiences in museums.
Aircraft turbine blades and expected advancement in technology using carbon n...
Gas turbines are of prime importance to aircrafts. The turbo machinery is a complex aspect of designing. Efficiency of turbo machinery is closely proportional to material selection and its performance. Each section of a turbo machinery deserves or has a different criteria of temperature dependency. As per this dependency turbine blades, nozzles and wheels are designed using different types of materials- alloys, which are highly resistant to temperature and light weight. This will lead to aircrafts which are very light and highly efficient. These materials are alloys which are very costly. And this high cost are making them difficult to be used abundantly. All these problems has made researchers to look around for material which is light, comparatively cheap and highly efficient as per turbine needs. This paper throws light on the existing materials used in turbine blades and a new compound which is a carbon allotrope which is capable of meeting all above needs perfectly.
Jean-Paul Gibson: Aerolab Subsonic Wind Tunnel Report
In this lab data was collected from (18) separate tap points along an airfoil within a subsonic wind tunnel generating winds at 70 miles per hour. In addition, this data was gathered for (4) different angles of attack.
The purpose of this lab was to calculate the pressure coefficient at each of those tap points. Our calculated results for the lab were compared to that of a manual that was provided for this experiment.
NASA 2004 report
The document discusses exploratory dynamic modeling of a nuclear-powered Brayton cycle system for a proposed Jupiter Icy Moons Orbiter (JIMO) mission. System integration is challenging because component models are often incompatible and simplified models must be used. The modeling effort used steady-state design data from reports on a 50MW reactor and 500kWe Brayton power conversion unit. A dynamic fuel pin model was coupled to a Brayton unit model based on equations from another report. Preliminary simulations showed an unintuitive reactor power increase when load decreased, consistent with other work, indicating a reactor control system would be needed. Further system integration work is still required for the JIMO project.
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3) For the buffet flow project, high-speed stereo PIV was used to investigate shock oscillations on a supercritical airfoil. Trailing edge turbulent eddies were suspected of generating
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Design Analysis Of Uav (Unmanned Air Vehicle) Using NACA 0012 Aerofoil Profile
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NACA 4412 Lab Report Final
This document summarizes experiments performed on NACA 4412 airfoils in Cal Poly's low speed wind tunnel. Three experiments were conducted: 1) force balance tests on two finite wings to determine coefficients, 2) pressure measurements on a full-span wing to calculate coefficients, and 3) wake rake tests to determine total drag coefficient. The force balance showed lift coefficient increasing pre-stall and dropping post-stall. Pressure data matched theoretical predictions and a NASA study. Lift was found to increase with angle of attack. The NACA 4412 performed best at low angles of attack, suited for a cruiser aircraft.
Naca 4 digit-delta
This document contains data points that define the profile of a NACA four-digit airfoil, including its maximum camber, position of maximum camber, thickness, and coordinates for 25 data points each on the upper and lower surfaces. It notes that cosine values were used to generate evenly spaced x-coordinates along the chord and explains that changing the number of data points would require manually adding or removing rows.
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• How contact-less magnetic position sensors are optimized for use in BLDC motor apps
• BLDC motor applications and key requirements in automotive and automation industries
PowerGen Africa Manuscript, Africa Energy Project Development Challenges
The document discusses challenges for developing energy projects in Africa. It identifies key challenges as: 1) rapidly growing energy demand driven by high GDP growth in some African nations, 2) assessing available fuel resources such as fossil fuels, hydro, wind, and solar, and 3) developing reliable transmission infrastructure to transport energy to demand centers. Additional challenges include securing financing, obtaining government support and addressing regulatory/environmental policies, and ensuring sufficient non-transmission infrastructure and labor. The document provides detailed analysis of different energy resources and considerations for assessment and development.
Aerodynamicsaeronauticsandflightmechanics 131107210632-phpapp01
This document provides an overview of aeronautics and aerodynamics. It begins with a brief history of manned flight, starting with the Wright Brothers' first sustained, powered flight in 1903. It then outlines several chapters that will cover topics in fluid mechanics, lift generation, drag forces, high-speed aerodynamics, aircraft propulsion systems, airplane performance, static and dynamic stability, and control. The document provides a table of contents to structure the topics and serves as an introductory guide to the principles of aeronautics.
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The artist creates digital aviation and bird posters using HDR photography and Photoshop techniques. They find aircraft to be works of art in themselves that can be beautiful, historic, perform amazing feats, or be scary. While warfare is scary, aircraft can also be beautiful and wondrous. The artist photographs various aircraft regardless of appearance and finds birds to be a subject that will remain even if aircraft cease to exist.
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The document summarizes the development and characteristics of several airfoil series developed by the National Advisory Committee for Aeronautics (NACA). It describes the early 4-digit and 5-digit series which used analytical equations to define airfoil shape based on camber and thickness. Later series like the 6-series used more advanced theoretical methods. The document provides details on naming conventions and equations used to define the geometry of airfoils within each series.
Naca 2415 finding lift coefficient using cfd, theoretical and javafoil
Abstract In this paper we have studied the experimental characteristic graph of NACA 2415.The experimental graphs were taken from the book, “Theory of wing section” by IRA H. ABBOTT. We used these graphs for the validation of our results. Then we use CFD to simulate the experimental flow conditions and check the results and compare them with the experimental results. We meshed the airfoil in ICEM CFD so that the meshing is very precise. We then calculate the NACA 2415 airfoil’s lift at different angle of attack theoretically and using CFD analysis and compare them with the experimental values. We find the errors between experimental and CFD values as well as experimental and theoretical values. We used another simulation software called Javafoil and used it for comparison. Keywords: Experimental, CFD, Theoretical, Javafoil
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The document discusses innovative sensor solutions from ams AG that are changing robotics. It describes how precise position sensors enable fine joint motor control for human-like robot movement. Vision sensors provide clear, undistorted images for robot vision. Environmental sensors allow robots to operate safely in difficult conditions. ams AG provides various sensor solutions for applications like position sensing, spatial sensing, image sensing, and environmental sensing to enable more advanced robotics.
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This chapter provides an overview of aircraft structure and components. It defines key terms like fuselage, wings, empennage, landing gear, and powerplant. It describes basic aerodynamic concepts like thrust, lift, weight, and drag. It explains how control surfaces like ailerons, elevators, and rudders control the aircraft's pitch, roll, and yaw. It briefly discusses different types of aircraft construction materials and methods.
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Este documento presenta el temario de la asignatura Sistemas e Instrumentos de Aeronaves. El curso analiza los componentes e instrumentación de las aeronaves, estudia los principales sistemas y su mantenimiento, y cubre el diseño básico de sistemas e instrumentos. El programa incluye sistemas de medición, datos de aire, actitud, navegación, motor, presentación de datos, sistemas integrados y características de diseño.
אירוע חנוכה עם חברת רובוטיקס
הרצאה על רובוטים מכל העולם
דוכני הרכבה והפעלה של חנוכיות מאירות
הדפסה בתלת מימד של סביבונים
סריגה! של רובוטים זוחלים
קרבות בין מכבים ליוונים בגירסה רובוטית
כרטיסי ברכה מנגנים ומאירים שכתובים בדיו מוליכה
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1) The document discusses two projects involving particle image velocimetry (PIV) - an analysis of fluid flow through a 90 degree pipe bend, and an identification of trailing-edge noise in buffet flows using high-speed PIV.
2) For the pipe bend project, PIV was used to capture images of fluid flow at different rates, showing dual vortices known as Dean Vortices. As flow rate increased, velocity in the upper right corner also increased while vortical structure diminished.
3) For the buffet flow project, high-speed stereo PIV was used to investigate shock oscillations on a supercritical airfoil. Trailing edge turbulent eddies were suspected of generating
AIRPLANES, SPACESHIPS, AND MISSILES: ENGINEERING LESSONS FROM FAMOUS PROJECTS
Slides from my Airbnb Tech Talk of June 5, 2013. Video at https://www.youtube.com/watch?v=sKTreDM4y-g&feature=youtu.be
Design Analysis Of Uav (Unmanned Air Vehicle) Using NACA 0012 Aerofoil Profile
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This research work is concerned with the application of conceptual design of Unmanned Air Vehicle (UAV). UAV is used for surveillance and reconnaissance to serve for the defense as well as national security and intelligence purpose. Here NACA 0012 aerofoil profile is used to design UAV by using CFD (Computational Fluid Dynamics) software. The aim of this research is to investigate the flow patterns and determine the aerodynamic characteristics of NACA 0012 profile by varying the angle of attack and Reynolds Number numerically. The research is carried out with symmetric aerofoil with the chord length of 0.1m. The research work explained different aerodynamic characteristics like lift force and drag force, lift and drag coefficient, pressure distribution over aerofoil etc.Professional Practice in Assistive Technology.
This document discusses how different human sensory, perceptual, cognitive, psychosocial, motor, and effector functions relate to assistive technology use. It provides examples of how assistive technologies can help those with visual impairments like blindness, cognitive impairments, and motor impairments that impact mobility. The document emphasizes that an individual's abilities and experience levels must be considered when designing and implementing assistive technologies.
NACA 4412 Lab Report Final
This document summarizes experiments performed on NACA 4412 airfoils in Cal Poly's low speed wind tunnel. Three experiments were conducted: 1) force balance tests on two finite wings to determine coefficients, 2) pressure measurements on a full-span wing to calculate coefficients, and 3) wake rake tests to determine total drag coefficient. The force balance showed lift coefficient increasing pre-stall and dropping post-stall. Pressure data matched theoretical predictions and a NASA study. Lift was found to increase with angle of attack. The NACA 4412 performed best at low angles of attack, suited for a cruiser aircraft.
Naca 4 digit-delta
This document contains data points that define the profile of a NACA four-digit airfoil, including its maximum camber, position of maximum camber, thickness, and coordinates for 25 data points each on the upper and lower surfaces. It notes that cosine values were used to generate evenly spaced x-coordinates along the chord and explains that changing the number of data points would require manually adding or removing rows.
Air boat
Air Boat is also known as Electric Boat.The military heavily used the air boats in submarines.No Pollution.No Fuel
Efficient Motor Commutation through Advanced Position Sensing - The Trend tow...
The session describes how contactless magnetic position sensors are optimized for use in high-speed brushless DC (BLDC) motors to meet reliability/efficiency requirements.
Attendees will learn:
• Major advantages of BLDC motors including higher efficiency, low noise, longer life, and higher reliability
• Key position sensing parameters and their relevance in the applications
• How contact-less magnetic position sensors are optimized for use in BLDC motor apps
• BLDC motor applications and key requirements in automotive and automation industries
PowerGen Africa Manuscript, Africa Energy Project Development Challenges
The document discusses challenges for developing energy projects in Africa. It identifies key challenges as: 1) rapidly growing energy demand driven by high GDP growth in some African nations, 2) assessing available fuel resources such as fossil fuels, hydro, wind, and solar, and 3) developing reliable transmission infrastructure to transport energy to demand centers. Additional challenges include securing financing, obtaining government support and addressing regulatory/environmental policies, and ensuring sufficient non-transmission infrastructure and labor. The document provides detailed analysis of different energy resources and considerations for assessment and development.
Aerodynamicsaeronauticsandflightmechanics 131107210632-phpapp01
This document provides an overview of aeronautics and aerodynamics. It begins with a brief history of manned flight, starting with the Wright Brothers' first sustained, powered flight in 1903. It then outlines several chapters that will cover topics in fluid mechanics, lift generation, drag forces, high-speed aerodynamics, aircraft propulsion systems, airplane performance, static and dynamic stability, and control. The document provides a table of contents to structure the topics and serves as an introductory guide to the principles of aeronautics.
Aircraft Presentation
The artist creates digital aviation and bird posters using HDR photography and Photoshop techniques. They find aircraft to be works of art in themselves that can be beautiful, historic, perform amazing feats, or be scary. While warfare is scary, aircraft can also be beautiful and wondrous. The artist photographs various aircraft regardless of appearance and finds birds to be a subject that will remain even if aircraft cease to exist.
The naca airfoil series
The document summarizes the development and characteristics of several airfoil series developed by the National Advisory Committee for Aeronautics (NACA). It describes the early 4-digit and 5-digit series which used analytical equations to define airfoil shape based on camber and thickness. Later series like the 6-series used more advanced theoretical methods. The document provides details on naming conventions and equations used to define the geometry of airfoils within each series.
Naca 2415 finding lift coefficient using cfd, theoretical and javafoil
Abstract In this paper we have studied the experimental characteristic graph of NACA 2415.The experimental graphs were taken from the book, “Theory of wing section” by IRA H. ABBOTT. We used these graphs for the validation of our results. Then we use CFD to simulate the experimental flow conditions and check the results and compare them with the experimental results. We meshed the airfoil in ICEM CFD so that the meshing is very precise. We then calculate the NACA 2415 airfoil’s lift at different angle of attack theoretically and using CFD analysis and compare them with the experimental values. We find the errors between experimental and CFD values as well as experimental and theoretical values. We used another simulation software called Javafoil and used it for comparison. Keywords: Experimental, CFD, Theoretical, Javafoil
Sensors Offer Infinite Opportunities for Designing Robots & Drones
The document discusses innovative sensor solutions from ams AG that are changing robotics. It describes how precise position sensors enable fine joint motor control for human-like robot movement. Vision sensors provide clear, undistorted images for robot vision. Environmental sensors allow robots to operate safely in difficult conditions. ams AG provides various sensor solutions for applications like position sensing, spatial sensing, image sensing, and environmental sensing to enable more advanced robotics.
Aircraft Structure - Chapter 2
This chapter provides an overview of aircraft structure and components. It defines key terms like fuselage, wings, empennage, landing gear, and powerplant. It describes basic aerodynamic concepts like thrust, lift, weight, and drag. It explains how control surfaces like ailerons, elevators, and rudders control the aircraft's pitch, roll, and yaw. It briefly discusses different types of aircraft construction materials and methods.
Aircraft Systems And Instruments Spanish
Este documento presenta el temario de la asignatura Sistemas e Instrumentos de Aeronaves. El curso analiza los componentes e instrumentación de las aeronaves, estudia los principales sistemas y su mantenimiento, y cubre el diseño básico de sistemas e instrumentos. El programa incluye sistemas de medición, datos de aire, actitud, navegación, motor, presentación de datos, sistemas integrados y características de diseño.
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Introduction to objective, scope and outcome the subject
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Levelling: Instrument used Object of levelling, Methods of levelling in brief, and Contour maps.
Chapter 4
Buildings: Selection of site for Buildings, Layout of Building Plan, Types of buildings, Plinth area, carpet area, floor space index, Introduction to building byelaws, concept of sun light & ventilation. Components of Buildings & their functions, Basic concept of R.C.C., Introduction to types of foundation
Chapter 5
Transportation: Introduction to Transportation Engineering; Traffic and Road Safety: Types and Characteristics of Various Modes of Transportation; Various Road Traffic Signs, Causes of Accidents and Road Safety Measures.
Chapter 6
Environmental Engineering: Environmental Pollution, Environmental Acts and Regulations, Functional Concepts of Ecology, Basics of Species, Biodiversity, Ecosystem, Hydrological Cycle; Chemical Cycles: Carbon, Nitrogen & Phosphorus; Energy Flow in Ecosystems.
Water Pollution: Water Quality standards, Introduction to Treatment & Disposal of Waste Water. Reuse and Saving of Water, Rain Water Harvesting. Solid Waste Management: Classification of Solid Waste, Collection, Transportation and Disposal of Solid. Recycling of Solid Waste: Energy Recovery, Sanitary Landfill, On-Site Sanitation. Air & Noise Pollution: Primary and Secondary air pollutants, Harmful effects of Air Pollution, Control of Air Pollution. . Noise Pollution Harmful Effects of noise pollution, control of noise pollution, Global warming & Climate Change, Ozone depletion, Greenhouse effect
Text Books:
1. Palancharmy, Basic Civil Engineering, McGraw Hill publishers.
2. Satheesh Gopi, Basic Civil Engineering, Pearson Publishers.
3. Ketki Rangwala Dalal, Essentials of Civil Engineering, Charotar Publishing House.
4. BCP, Surveying volume 1
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