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MultiElement Airfoils is Listed Among
SAE
Aerospace Engineering Magazine
"Top Products for 2003".
Summary
The airfoil shape can make or break your wing design and overall
airplane performance. For slow takeoffs and landings, you need a high lift
section such as a multi-element airfoils shape. At the same time for efficient
flying at altitude, you need a low drag airfoil. MultiElement Airfoils is
the only tool that you need to resolve these conflicting airfoil design
problems.
MultiElement Airfoils 4.1 is a state-of-the-art CFD
tool for airfoil analysis that puts the power of airfoil selection and design
at your fingertips. It gives you the ability to consider any airfoil
shape that would make your design a reality. This is because the software
incorporates the most powerful CFD methods in an easy-to-use interface. No
other airfoil analysis software provides the features of MultiElement Airfoils
to expedite the airfoil design and analysis process.
MultiElement Airfoils 4.1 solves the compressible Euler &
Navier-Stokes equations for arbitrarily placed objects. It is a turn-key
product that eliminates grid generation hassles and accurately computes lift,
drag and moments for a group of airfoils and individual airfoils within the
group. MultiElement Airfoils displays graphs of pressure, Mach number,
temperature and total pressure using built-in post processing tools (it does
not require additional third party software for pre or post processing).
It is an excellent tool for optimizing cross-sectional shapes and getting
the correct placement of aerodynamics components for aircraft, automobiles,
boats, house hold products and other equipment.
MultiElement Airfoils is a computational fluid dynamics (CFD)
software package that automatically analyzes the full gamit of airfoil
shapes and configurations. It solves isolated and multiple shapes in subsonic,
transonic and supersonic flows. It offers the following benefits:
Benefits
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Solve conflicting wing design problems that call for high lift at
landing and takeoffs but low drag and efficiency in the cruise
configuration.
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Solve the problem of generating high lift when the wing dimensions
are fixed by the rules of the competition.
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Analyze multiple airfoils shapes without the hassles of grid generation.
Just drag the airfoils into place (or enter their exact location), size and
rotate them and click the menu to automatically generate your grid.
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Accurately solves compressible Euler & Navier-Stokes equations
for for multiple airfoils and other 2-dimensional shapes.
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Understand the behavior of airfoils used in the design of wings,
helicopter blades, hydrofoils, fans, propellers and other equipment.
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Understand and make critical design decision in transonic & supersonic
flow regime.
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Easy-to-use tool for designing more efficient wing & machine blade
cross-sections.
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Eliminate steep learning curve for new engineers & reduce training
costs.
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Windows based interfaces requires little or no training.
Compressible Flow Solver
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2-dimensional compressible Navier-Stokes Equations for laminar
flows
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2-dimensional compressible Euler equations using a finite-volume
solver
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Boundary layer equations using edge velocity from Euler equations
solver
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Option for axisymmetric equations & boundary conditions
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2nd order flux vector splitting
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4-stage Runge-Kutta time marching scheme using local time steps
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Automatic cartesian grid generation for arbitrary multiple body
placement.
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Plots of pressure, Mach number, temperature & total pressure
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Surface plots of Cp, Cf, Mach number, velocity ratio &
temperature
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Computation of overall lift, drag & moment coefficients about
arbitrary locations on and off the airfoils.
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Computation of lift, drag & moment coefficient for each
shape.
Incompressible Flow Solver
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Linear strength vortex panel method
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Coupled boundary layer solver
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Lift, drag & moment coefficient calculations for individual
airfoils
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Prediction of transition & separation points
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Stall & maximum lift prediction
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Surface graphs of pressure & velocity ratio
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Contour graphs of Cp
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Graphs of Cl, Cd & Cm versus angle of attack
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Graphs of Cl vs Cd.
Other Features of MultiElement Airfoils
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Incompressible flow solver using vortex panel method coupled with
boundary layer solver
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Compressible flow solver based on Euler Equations and Navier-Stokes
Equations
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Built-in library of NACA 4, 5 & 6-digit airfoils
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Custom airfoil analysis
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Computes Cl, Cd & Cm
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Stall Model for potential flow solver
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Built-in graphs
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Built-in tables
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Export tables to .csv files
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Export airfoil to .dxf files
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Airfoil plotting
Applications
New!
Compressible
Navier-Stokes solutions
Euler equations solutions
Airfoil icing & microtab
studies
Click here
for high speed jet over airfoils (blown wing/flap
application)
Click here for race car wing
example.
Click here for stability
analysis.
Requirements
MultiElement Airfoils requires a PC with a Pentium 120 or later running
Windows 95 or later and a connection to the internet.
| * The Leased & Floating Versions Require
Internet Connection to access the software. The lease period
starts after the second (2nd) access of the software. Users can use
the software on any internet connected PC running Windows 95 or later
(Windows XP preferred). |
| Telephone Your Orders:
Please call us at (352) 687-4466 to place your credit card order by
telephone. We can provide you with a download URL & password after
the transaction is processed. |
| Fax Your Orders:
Please click here
to fax your order. (.pdf order form) |
Support and Upgrades
We provide free technical support and upgrades for up to one year
after purchase for our perpetual license packages. The leased versions of
the software can be obtained from our site soon after they are updated.
Get Started Now
Find out how MultiElement Airfoils help you with your current project.
Please click here
to contact us or call us at (352) 687-4466.
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