AerofoilJobs
Vær venlig at Tilmelde dig eller Log ind for at se detaljer.
Vær venlig at Tilmelde dig eller Log ind for at se detaljer.
Vær venlig at Tilmelde dig eller Log ind for at se detaljer.
I essentially need 3 aerofoil shaped wings attached to each other in CAD software.
Vær venlig at Tilmelde dig eller Log ind for at se detaljer.
Design aerofoil, AoA, and diameter for 2kW Darrieus type wind turbine. This will require a bit more than mechanical engineering. Even the "wing" profile will need to be analysed. I don't know if it needs a symetrical, semi-symetrical, or fully cambered section. Also, for the power, both blade length and turbine diameter will need to be defined. I don't actually need structural analysis, "just" fluid dynamics.
use solidwroks draw two 3D model of aerofoil, one is basic model, the other one is designed model( this model need change some dimensions) , then do simulation by ANSYS, the parameter need include turblence, area change and angle change to check the lift. the result and report need provided.
i have aerofoil. need cfx analysis in 1 hr. or earlier
I need someone who is good at Solidworks and Ansys To design 2 radiators picture will be added below and you can improvise on the measurements Both radiators will be almost similar with minor changes to fin design 1. First radiator will be with a W fin design and the second will have more of an aerofoil design 2. Run CFD Optimization for the first design only to calculate drag and heat dissipation
I need someone who is good at Solidworks and Ansys To design 2 radiators picture will be added below and you can improvise on the measurements Both radiators will be almost similar with minor changes to fin design 1. First radiator will be with a W fin design and the second will have more of an aerofoil design 2. Run CFD Optimization for the first design only to calculate drag and heat dissipation
The model used, is a scale TARF model, a modern looking hatchback (Figure 1). The CAD model used in this investigation was also used to create the scale model you have already used in the wind tunnel experiment. The geometry of the rear wing is available and can be added to the model. The wing provided is based on the GOE244 aerofoil profile. The students will perform the CFD analysis on the given model in order to measure aerodynamic forces and moments, understand how the wing angle of attack influences the aerodynamic performance and isolate the influence of the supporting apparatus (used in the experimental analysis) on the results. The outcome of this assignment will be a report.
Hey Joseph, I got a coursework which deadline is at 24 of this month, is regarding simulation of an aerofoil, can you help me with it?
Hey, I got CFD cw due to 24 of this month which should include Star CCM+ software work and matlap, basically aerofoil simulation. Can you help me with it?
Hey, I got CFD cw due to 24 of this month which should include Star CCM+ software work and matlap, basically aerofoil simulation. Can you help me with it?
Hey, I got CFD cw due to 24 of this month which should include Star CCM+ software work and matlap, basically aerofoil simulation. Can you help me with it?
Hi Mohamed M., I noticed your profile and would like to offer you my project. We can discuss any details over chat. Project Subject: Design of an aerofoil under certain environmental circumstances.
Hi Jehan H., I noticed your profile and would like to offer you a project. We can discuss any details over chat. Project Subject: Design of an aerofoil under certain environmental circumstances.
We do an 2d aerofoil simulation by using a software star ccm +. With small reports. I am choosing boeing of air flow over an aerofoil You will work in groups of three to perform a comparison of the properties of three aerofoil shapes, based on CFD simulations in two-dimensions, at an air speed of 50 m/s. In your report you should include details of the simulation such as grid shape and size, grid convergence, residual behaviour, and the input parameters for the simulation. You should also present the results of your simulations indicating aspects such as air flow over the wing section, pressure variations and lift and drag coefficients. In particular you should investigate and compare the performance of the wings at different angles of attack. Each group should consid...
I need a mesh generation done for 2D aerofoil while on a conference call. The details are attached. It must be done on ICEM CFD and no other softwares
I have a project that needs to be done, The results have been done using ansys, I need a litretarue view, methodology, discussion and conclusion to be done. I used K-omega SST model and run results for NACA 0012 and NACA 0018, at angles of attack 4, 6, and 8. The project is 6000 words.
I have a project that needs to be done, it is using ansys to run models on 2 different aerofoils to determine which aerofoil shape is the most optimum for wind turbines. Need a methodology, results, discussion and conclusion.
I need to make calculation of lift and drag forces on Aerofoil NACA0015 by hand, later make an Ansys simulations and afterwards a report according with predictions, and behavior between them and finallly a conclusion.
I HAVE A project of cfd run a simulation for flow over aerofoil wings if any one interested please send message i will share the rest of the details.
Calculate life of an aerofoil.
Some mechanical design needs to be draw on Ansys. Will send you more details regarding aerofoil,cylinder, etc.
Some mechanical design needs to be draw on Ansys. Will send you more details regarding aerofoil,cylinder, etc.
The AF10 airflow bench is a simple miniature wind tunnel; it provides a controlled airstream for experiments which use matching test equipment. The AF10 airflow bench comprises a fan which draws air from the atmosphere and delivers it along a pipe to an airbox which is above the test area. In the pipe there is a valve which may be used to regulate the discharge from the fan.
Hi sorry for the delay. Please bid on the project named' analysis of flow on a clark aerofoil'
- In this lab, the flow over a Clark Y aerofoil is modelled. The flow is assumed to be twodimensional, viscous and turbulent. The effect of variation of the angle of attack has on the lift and drag characteristics of the aerofoil are the main object of this lab as well as the utilizationof different turbulence models when separation occurs for high angles of attack. Additional details and the geometry will be provided.
#Aerofoil should be clearly idintified #the volume of the seed wing should be calculated #The total volume of the seed should also be calculated #Budget 50USD #SLDPRT or Ansys compatible file should be delivered
LEASE READ THIS AND REPLY ME IF PROJECT CAN BE COMPLETED #Aerofoil should be clearly idintified #the volume of the seed wing should be calculated #The total volume of the seed should also be calculated #Budget 20USD #SLDPRT or Ansys compatiable file should be delivered
LEASE READ THIS AND REPLY ME IF PROJECT CAN BE COMPLETED #Aerofoil should be clearly idintified #the volume of the seed wing should be calculated #The total volume of the seed should also be calculated #Budget 20USD #SLDPRT or Ansys compatiable file should be delivered
LEASE READ THIS AND REPLY ME IF PROJECT CAN BE COMPLETED #Aerofoil should be clearly idintified #the volume of the seed wing should be calculated #The total volume of the seed should also be calculated #Budget 20USD #SLDPRT or Ansys compatiable file should be delivered .
Hi Amandeep M., I noticed your profile and would like to offer you my project. We can discuss any details over cLEASE READ THIS AND REPLY ME IF PROJECT CAN BE COMPLETED #Aerofoil should be clearly idintified #the volume of the seed wing should be calculated #The total volume of the seed should also be calculated #Budget 20USD #SLDPRT or Ansys compatiable file should be delivered hat.
I want someone to simulate a flow around an aerofoil with and without gurney flaps. Who has a strong knowledge of aerodynamics to solve a problem and simulate it.
I want you to run simulations on ansys or openfoam and calculate lift, drag and animations of velocity profile of a moving aerofoil in a laminar flow.
I am a engineering student of Mechanical branch and i need your help for making few simulations for oscillating aerofoil and studying drag and lift on the aerofoil Please reply as soon as possible Ready to pay
Laboratory experiment about investigate the variation in pressure around the aerofoil at different angles of incidence and the resultant effect on lift coefficient. The particular aerofoil to be tested is a symmetrical, constant cross-section RA 104 airfoil of 10% thickness. 1- Introduction about fundamental operation of an aerofoil (100 words mix) 2- The job is to compare between 6 tables recorded and convert the data to Si units. 3- Produce a plot of CL (Coefficient Lift) versus angle of incidence. 4- Present the Reynolds number associated with the test. 5- Provide discussion of (the effect of increasing the angle of incidence, the distribution of pressure around the aerofoil, and on the lift coefficient) 6- Discuss the contribution of estimated pot...
Laboratory experiment about investigate the variation in pressure around the aerofoil at different angles of incidence and the resultant effect on lift coefficient. The particular aerofoil to be tested is a symmetrical, constant cross-section RA 104 airfoil of 10% thickness. 1- Introduction about fundamental operation of an aerofoil (100 words mix) 2- The job is to compare between 6 tables recorded and convert the data to Si units. 3- Produce a plot of CL (Coefficient Lift) versus angle of incidence. 4- Present the Reynolds number associated with the test. 5- Provide discussion of (the effect of increasing the angle of incidence, the distribution of pressure around the aerofoil, and on the lift coefficient) 6- Discuss the contribution of estimated pot...
Laboratory experiment about investigate the variation in pressure around the aerofoil at different angles of incidence and the resultant effect on lift coefficient. The particular aerofoil to be tested is a symmetrical, constant cross-section RA 104 airfoil of 10% thickness. 1- Introduction about fundamental operation of an aerofoil (100 words mix) 2- The job is to compare between 6 tables recorded and convert the data to Si units. 3- Produce a plot of CL (Coefficient Lift) versus angle of incidence. 4- Present the Reynolds number associated with the test. 5- Provide discussion of (the effect of increasing the angle of incidence, the distribution of pressure around the aerofoil, and on the lift coefficient) 6- Discuss the contribution of estimated pot...
i want a report about wing, lift and Bernoulli pressure and lift coefficients of a thin airfoil, and the effect of the variation in pressure around the aerofoil at a deferent angel of attack and the resistance effect on the lift coefficient.
...employee & 25+ part time. Now we have huge work flow & that's why we are searching some freelancer from outside for few tasks. See the attached task: Type: CFD (need to Use Ansys Workbench) (just need to do for 0 degree) Task: Experiment Deadline: 30 Oct Friday night or 31 Oct asap..... Find Attached. Experiment is already done and data is included as image. You just need to make an aerofoil with 0 degree wake...... and write the report with experiment description, CFD analysis from Ansys with conclusion drawn from that supported by necessary discussion. NB: Referencing has to be in harvard do not copy paste from the given sheet to write experiment description, always use paraphrasing. As you do not need to do analysis for all angles from 0 to 20...
...employee & 25+ part time. Now we have huge work flow & that's why we are searching some freelancer from outside for few tasks. See the attached task: Type: CFD (need to Use Ansys Workbench) (just need to do for 0 degree) Task: Experiment Deadline: 30 Oct Friday night or 31 Oct asap..... Find Attached. Experiment is already done and data is included as image. You just need to make an aerofoil with 0 degree wake...... and write the report with experiment description, CFD analysis from Ansys with conclusion drawn from that supported by necessary discussion. NB: Referencing has to be in harvard do not copy paste from the given sheet to write experiment description, always use paraphrasing. As you do not need to do analysis for all angles from 0 to 20...
This project is about creating a 3D modelling of a flexible aerofoil, this also include all the electronic parts inside the Aerofoil, which consist of servos, actuators and etc.
With provided parameters, design 3D model of small vertical axis wind turbine VAWT with 3 bladed aerofoil which rotates counter clockwise CCW using standard parts with identified parts suppliers list. The same task for CW VAWT The same task for CCW HAWT The same task for CW HAWT
I need you to work on how to improve the design of the current aerofoil designs. I have flexibility in time. Thanks!
Need a complete CFD simulation using Ansys v15 on a 3D aerofoil with end plates and a ground effect. Two simulations to be completed, one with a rear wing with a single element and the second with duel element. A detailed proceedure report is to be writen on the important steps taken in order to complete an accurate simulation (E.g how the domain was created, what skewness and orthgon quality was used, mesh quality) This ^ has been completed by manufacturing the wing and end plates tested in wind tunnel , results are to be compaired with CFD. A good experience in CFD and report writing is essential. If given the job more information will be given.
Need to complete a CFD analysis on a Naca 64(2)-415 to aquire aerodynamic properties of the aerofoil. Modifications need to made in a second simulation in order to create a better aerofoil. If you feel able to complete this task imbox me for further detail.
I need someone to design high lift low drag aerofoils, for a unmanned application ideally a candidate that can design the airframe aswell will be best suited for this project. please only european/north american designers due to confidentiality
