This is the Windows app named Xoptfoil to run in Windows online over Linux online whose latest release can be downloaded as Xoptfoil-v1.11.1-windows.zip. It can be run online in the free hosting provider OnWorks for workstations.
Download and run online this app named Xoptfoil to run in Windows online over Linux online with OnWorks for free.
Follow these instructions in order to run this app:
- 1. Downloaded this application in your PC.
- 2. Enter in our file manager https://www.onworks.net/myfiles.php?username=XXXXX with the username that you want.
- 3. Upload this application in such filemanager.
- 4. Start any OS OnWorks online emulator from this website, but better Windows online emulator.
- 5. From the OnWorks Windows OS you have just started, goto our file manager https://www.onworks.net/myfiles.php?username=XXXXX with the username that you want.
- 6. Download the application and install it.
- 7. Download Wine from your Linux distributions software repositories. Once installed, you can then double-click the app to run them with Wine. You can also try PlayOnLinux, a fancy interface over Wine that will help you install popular Windows programs and games.
Wine is a way to run Windows software on Linux, but with no Windows required. Wine is an open-source Windows compatibility layer that can run Windows programs directly on any Linux desktop. Essentially, Wine is trying to re-implement enough of Windows from scratch so that it can run all those Windows applications without actually needing Windows.
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Xoptfoil to run in Windows online over Linux online
DESCRIPTION
Airfoil optimization using the highly-regarded Xfoil engine for aerodynamic calculations. Starting with a seed airfoil, Xoptfoil uses particle swarm, genetic algorithm and direct search methodologies to perturb the geometry and maximize performance. The user selects a number of operating points over which to optimize, desired constraints, and the optimizer does the rest.Features
- Supports up to 30 operating points during optimization and multiple user-defined constraints
- Each operating point has a specified lift coefficient or angle of attack, Reynolds number, Mach number, and flap deflection
- Flap angle for each operating point can be used as design variables
- Different optimization objectives (minimize drag, maximize glide slope, minimize sink rate, or maximize lift) can be set at each operating point
- Each operating point is assigned a relative weight (importance) by the user
- Available constraints include thickness, camber, curvature reversals, pitching moment, and trailing edge wedge angle
- Currently included optimization algorithms: particle swarm, genetic algorithm, and Nelder-Mead simplex algorithm
- The optimizer is robust: many checks for reasonable geometry and Xfoil consistency in place
- Parallel version available
- Xfoil engine accurately predicts transition, separation bubbles, and stall at low Reynolds numbers
Audience
Aerospace
User interface
Console/Terminal
Programming Language
Fortran
This is an application that can also be fetched from https://sourceforge.net/projects/xoptfoil/. It has been hosted in OnWorks in order to be run online in an easiest way from one of our free Operative Systems.
