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$10 USD / hour
Flag of PAKISTAN
karachi, pakistan
$10 USD / hour
It's currently 11:35 PM here
Joined June 24, 2019
0 Recommendations

Enayat R.

@EngrEnayatRaza

 5.0 (18 reviews)
4.2
4.2
100%
100%
$10 USD / hour
Flag of PAKISTAN
karachi, pakistan
$10 USD / hour
95%
Jobs Completed
90%
On Budget
90%
On Time
43%
Repeat Hire Rate

Solution Provider of Engineering Software Projects

Solution Provider of Engineering Software Projects. ●Data Science & Machine Learning ●Engineering Maths, Calculus, Algebra & Differential Eqns ●GUI Designing ●Numerical Methods/Techniques ●Digital Signal Processing ●Optimization & Curve Fitting ●Feedback Control Systems ●Image Processing ●Electronic Circuits ●Electrical Networks ●Mechanical Models ●Telecommunication and Much More !
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Portfolio

5520402
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
5515072
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
5513113
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
5513242
* 'LABVIEW' - GUI/HMI Model Building Task. * the task is to develop a working labview program which depicts set point achieving model. * the required labview model allows a user to enter his set point value and then automatically achieves that value on output by using set of required logical and numerical operators. * user will enter his desired setpoint value by moving the setpoint input knob onto his desired figure. * as the user moves the setpoint knob on his desired value, its exact value is displayed on a digital meter which is present very next to setpoint knob. * there is an input 'guage' which moves and points to that exact setpoint value. * there is a input 'tank cell' which fills and reach to that exact setpoint value. * similarly on the output side there are 'output knob' , 'output digital meter' , 'output guage' , 'output led indicator' and 'output tank cell'. * these all will show the achieved point value on its output.
LABVIEW - GUI/HMI Model Building Task
* 'LABVIEW' - GUI/HMI Model Building Task. * the task is to develop a working labview program which depicts set point achieving model. * the required labview model allows a user to enter his set point value and then automatically achieves that value on output by using set of required logical and numerical operators. * user will enter his desired setpoint value by moving the setpoint input knob onto his desired figure. * as the user moves the setpoint knob on his desired value, its exact value is displayed on a digital meter which is present very next to setpoint knob. * there is an input 'guage' which moves and points to that exact setpoint value. * there is a input 'tank cell' which fills and reach to that exact setpoint value. * similarly on the output side there are 'output knob' , 'output digital meter' , 'output guage' , 'output led indicator' and 'output tank cell'. * these all will show the achieved point value on its output.
LABVIEW - GUI/HMI Model Building Task
5520835
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
5520370
* 'MATLAB - GUI (GRAPHICAL USER INTERFACE) TASK'. * gui contains two buttons ('load' button & 'save' button), a plot window and two numeric output text boxes ('ARI' textbox and 'HeartRate' textbox). * a csv data file is provided in which patient doppler data is present. * at first user clicks 'load' button; this will read the data from the given excel file. * after the file has read, required plot of 'velocity vs time' is displayed on plot window of GUI. * also calculate 'ARI' (arterial resistivity index) and 'HeartRate' by using their provided formulae and simultaneously show both the calculated values on their respective text boxes on GUI. * after the plot and numeric values (ARI & HeartRate) are displayed on the GUI, user now will click 'save' button; this will print both the calculated values (ARI & HeartRate) on command window and along with that also generate a text file named 'DopplerResults.txt' in which it will print and save the two calculated values (ARI &
MATLAB - GUI (GRAPHICAL USER INTERFACE) TASK
5520402
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
* 'Embedded Microcontroller Programming Task - Arduino Mega - AVR Coding - ATMega2560'. * the task is to do programming for the quadcopter's subsystem: 'Light Illumination Sensing Subsystem'. * Voltage levels in the range 0 – 2Volts will be considered as poor illumination. In that case the red LED should turn on. * Voltage levels in the range 2 – 2.5Volts will be considered as marginal illumination. In that case the yellow LED should turn on. * Voltage levels in the range 2.5 – 5Volts will be considered as good illumination. In that case the green LED should turn on. * In the case of poor illumination, the RGB LED should illuminate a white color in full intensity, and the buzzer should make a beeping sound every 100msec. * In the case of adequate illumination, the buzzer should make a beeping sound every 250msec. * In the case of good illumination, the buzzer and the RGB LED should be turned off.
Embedded Microcontroller Programming Task - Arduino Mega
5515072
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
* SOLIDWORKS - Motor Cage/Casing – 3D Model Designing Task: * the task is to design a 'motor cage/casing'. * casing overall dimensions are given. * followed every major and minor detailing that are asked to be made while producing the model. * required 3D model of 'motor cage/casing' with exact dimensions is made.
SOLIDWORKS - 3D CAD Model Designing Task
5513113
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
* ANSYS - FEA SIMUATLION TASK: * the task is to 'design' and then perform 'FEA simulation' (finite element analysis) to any component of an aircraft of our choice. * the chosen component is 'aerofoil/rudder'. * aerofoil is first designed in 2D by using 'aerofoil-e168' design coordinates. * then this 2D design of rudder is converted into 3D with defined dimensions of its length, width and height. * after the 3D rudder model is created, we apply material to it i.e. 'steel'. * then meshing is applying on rudder model with standard mesh size so that the whole aerofoil model is discretized into smaller finite elements. * then applying 'boundary conditions' and 'loading conditions' to the meshed rudder model. * finally applying simulations and getting the required simulation outputs i.e. 'total deformation' , 'shear stress' and 'von misses'. * also writing a detailed explanatory report highlighting each and every stage with snapshots.
ANSYS - FEA SIMUATLION
5513242
* 'LABVIEW' - GUI/HMI Model Building Task. * the task is to develop a working labview program which depicts set point achieving model. * the required labview model allows a user to enter his set point value and then automatically achieves that value on output by using set of required logical and numerical operators. * user will enter his desired setpoint value by moving the setpoint input knob onto his desired figure. * as the user moves the setpoint knob on his desired value, its exact value is displayed on a digital meter which is present very next to setpoint knob. * there is an input 'guage' which moves and points to that exact setpoint value. * there is a input 'tank cell' which fills and reach to that exact setpoint value. * similarly on the output side there are 'output knob' , 'output digital meter' , 'output guage' , 'output led indicator' and 'output tank cell'. * these all will show the achieved point value on its output.
LABVIEW - GUI/HMI Model Building Task
* 'LABVIEW' - GUI/HMI Model Building Task. * the task is to develop a working labview program which depicts set point achieving model. * the required labview model allows a user to enter his set point value and then automatically achieves that value on output by using set of required logical and numerical operators. * user will enter his desired setpoint value by moving the setpoint input knob onto his desired figure. * as the user moves the setpoint knob on his desired value, its exact value is displayed on a digital meter which is present very next to setpoint knob. * there is an input 'guage' which moves and points to that exact setpoint value. * there is a input 'tank cell' which fills and reach to that exact setpoint value. * similarly on the output side there are 'output knob' , 'output digital meter' , 'output guage' , 'output led indicator' and 'output tank cell'. * these all will show the achieved point value on its output.
LABVIEW - GUI/HMI Model Building Task
5520835
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
* 'Ordinary Differential Equation (ODE) Solver' Task. * task1 is to solve 'predator-prey population model' (involves two distinct populations: 'foxes as predators' and 'rabbits as prey') using ODE solver solver and produce the required corresponding number of output plots of 'population vs time'. * task2 is to solve 'Zombie Outbreak model' (involves three distinct populations: 'humans' , 'zombies' and 'deads') using ODE solver and produce the required corresponding number of output plots of 'population vs time'.
Ordinary Differential Equation (ODE) Solver Task.
5520370
* 'MATLAB - GUI (GRAPHICAL USER INTERFACE) TASK'. * gui contains two buttons ('load' button & 'save' button), a plot window and two numeric output text boxes ('ARI' textbox and 'HeartRate' textbox). * a csv data file is provided in which patient doppler data is present. * at first user clicks 'load' button; this will read the data from the given excel file. * after the file has read, required plot of 'velocity vs time' is displayed on plot window of GUI. * also calculate 'ARI' (arterial resistivity index) and 'HeartRate' by using their provided formulae and simultaneously show both the calculated values on their respective text boxes on GUI. * after the plot and numeric values (ARI & HeartRate) are displayed on the GUI, user now will click 'save' button; this will print both the calculated values (ARI & HeartRate) on command window and along with that also generate a text file named 'DopplerResults.txt' in which it will print and save the two calculated values (ARI &
MATLAB - GUI (GRAPHICAL USER INTERFACE) TASK

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1.0
$100.00 USD
Project 27860916 has been deleted
I forget my money for this project. He ask half of payment without complete and after release he blocked my chat message. He is terrible freelancer on here. Don't hire this scamed freelancer. Now i am going to refund my money with freelancer support. I recommend this scamed freelancer.
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Closed User
@aleksandrruban
•
4 years ago
5.0
$225.00 USD
Electrical Engineering Project
Thank You So Much !!!
Engineering
Electronics
Matlab and Mathematica
Mechanical Engineering
Electrical Engineering
P
Flag of Kopal S.
@Professional1980
•
4 years ago
4.8
$100.00 USD
ECG data bit flip
Good work Enayat, hope to work with you soon
Engineering
Matlab and Mathematica
Algorithm
Electrical Engineering
Mathematics
N
Flag of Naveed N.
@Navnaw
•
4 years ago
5.0
$40.00 USD
MATLAB SIGNAL PROCESSING
Thank you so much. Great knowledge and very supportive person. I recommend him highly.
Engineering
Matlab and Mathematica
Algorithm
Electrical Engineering
Mathematics
P
Flag of Kopal S.
@Professional1980
•
4 years ago
5.0
$22.00 USD
SOLIDWORKS MECHANICAL PARTS AND ASSEMBLY -- 2
As always, excellent work done by Enayat R
Engineering
CAD/CAM
Solidworks
Mechanical Engineering
Assembly
R
Closed User
@RadhikaJoshi065
•
4 years ago

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