Sunday, May 27, 2012

Analyze, Print & Export NACA Airfoils

A limited edition version of VisualFoil 5.0 is now available for the price of $29.
 
 
This version allows the analysis of NACA 4, 5 and 6-digit airfoils using the built-in library. In addition, the airfoils can be modified within the program and exported to ASCII (text) or .dxf file formats.
 
VisualFoil 5.0 uses a linear strength vortex panel method coupled with boundary layer analysis solver  to compute lift, drag and moment coefficients for subsonic (Prandtl-Glauert correction) and incompressible flows past airfoils. The stall model allows the estimation of the angle of maximum lift. Graphs of Cl vs angle of attack, Cl vs Cd and other curves are available within the software and can be exported to external reports.
 
 
 

More information about VisualFoil can be found at: http://www.hanleyinnovations.com/vf50.html
 
VisualFoil 5.0 is excellent for:
  • accurate airfoil analysis and computing lift, drag and moment coefficients
  • NACA 4, 5 & 6-Digit Airfoil library 
  • student projects (aircraft, wind energy, hydrofoils)
  • an inexpensive airfoil reference tool
  • classroom demonstrations
  • printing airfoils templates on a Windows supported printer
  • exporting accurate representations of airfoils to .dxf files  
The NACA-Version of VisualFoil requires a PC or Laptop running Windows XP, Vista or Version 7. The purchase price is $29 US.

Please use the following link to purchase the software.

https://www.paypal.com/cgi-bin/webscr?cmd=_s-xclick&hosted_button_id=36LHRSAZ2B6W2

Do not hesitate to contact me at (352) 249-3658 if you have any questions.

Thanks for reading.

Monday, May 21, 2012

Setting Sails

It is important to realize that sails are wings and they often act like wings (this applies to almost any sail and not just rigid wing sails now popular in the America's Cup race). Therefore, when it is required to optimize the sail settings for a specific boat, we can rely on our knowledge of wing aerodynamics and our bag of accumulated tricks (experience & tools) to do an efficient job.

The primary goal of sail optimization is to increase the lift (for a good drive force component) and reduce the drag (stability must be maintained during the process).  Sail optimization is a repetitive job.  This is because, like wings, the drive force of the sail in up-wind sailing depends on the apparent wind vector (direction and magnitude), the planform (area & aspect ratio), the camber (flat or curved cross sections), the gap between the fore and main sails, the mast and other parameters (such as height above the deck, hull shape, etc.).

Stallion 3D Simulation of flat thin sails. The graphs shows pressure.

A good design does not simply mean infinite aspect ratio to reduce tip vortices (tip vortices increase drag as seen in above picture).  The heeling moment will be too big (unless, of course, you have this installed on your boat).  Large camber or deeper sails can increase the drive force, however, stability and drag from supporting underwater devices (keel and rudder) can erode this advantage. To obtain the optimal (or best we can do at the moment) specifications for a particular sail, we must test our design iterations against a number of possible sailing conditions. 

Stallion 3D Simulation of cambered thin sails. 

Deadlines are the natural enemy of testing and optimization.  Experimental setup and testing in a wind tunnel can be time consuming and costly (and might even require a minor in wood carving).  Wind tunnel and tow-tank test can be made more efficient and cost-effective only if the most promising designs are tested prior to making the final decision.

Stallion 3D Simulation of cambered thin sails with a larger angle between jib and main sail.

Computational methods can be used to test conceptual and preliminary design ideas.  However, a good understanding of the assumptions used in a particular method is required to get useful information to test in the wind tunnels and water tanks.  What is the difference between 2D sections, vortex lattice, panel methods, Euler/Navier-Stokes methods? They are all useful.   Knowing the answer and how to apply the various concepts in a concerted manner can speed up your upwind sail to the best design.

No sail optimization study is complete without the consideration of the underwater systems (keel, rudders and other appendages). Like sails, keels and rudders are wings and also behave as wings.  The goal to provide stability and lateral resistance can result in drag (induced and profile).  Also, an efficient keel for up-wind sailing can be terrible otherwise.  In short, sail and keel/rudder analysis are coupled and equal partners in sailboat optimization.

Stallion 3D simulation of a keel and bulb.

In the area of aerodynamics conceptual design, a lot of nautical mileage can be quickly covered with a tool that has a built-in set of realistic physical assumptions, automatic grid generation and cost effective and readily available computing platform.  Stallion 3D can be deployed on an ordinary Windows PC, run in multiple directories to take advantage of multi-core processing and efficiently and accurately analyze the most difficult models.

Stallion 3D simulation of sails and hull (3D model from http://turbosquid.com).
Graph shows surface speed in m/s.

More information can be found at http://www.hanleyinnovations.com/stallion3d.html.  The cost of a 3-months lease of Stallion 3D is $895.

Thanks for reading. 

Do not hesitate to email or call me at (352) 240-3658 if you have any questions.

Tuesday, May 15, 2012

Faster Target Drones

Transonic jets are not easy targets and valuable training and experience can be gained by using faster drone aircraft as targets during training. 

Transonic & supersonic jets make very expensive drones. One solution is to use outdated airplanes as targets.  However, retrofitting these airplanes with new equipment can be equally expensive especially in light of their inevitable fate.

A cost reducing solution is to modify existing target UAVs so they can efficiently fly at higher Mach numbers with relatively inexpensive propulsion systems.  This requires drag reducing techniques at the regime of flight in the neighborhood of the drag divergence Mach number aka Mdd.

Stallion 3D Simulation of UAV at M=0.95

Drones designed for subsonic flight look and behave differently than those designed for supersonic flight.  A proven method for increasing the Mdd is to sweep back the main wings.  However, if an existing UAV is redesigned with a swept wing, the stability and flight characteristics of the aircraft will change and the cost of the modifications can increase.  

Stallion 3D was used for a quick design study with  four  different Mach numbers near Mdd and two similar UAVs to test the concept of airfoil modification as apposed to sweep to improve the aircraft performance at high transonic Mach numbers.  

Grid generation for the aircraft was automatic and the total set of calculations (8 separate cases) was completed in under 12 hours on a 4-core laptop computer running Windows 7.

Existing UAV System with Modified Airfoil at Mach number of 0.7, 0.8, 0.9 & 0.95.



Existing UAV System with Modified Wing Sweep at Mach numbers of 0.7, 0.8, 0.9 & 0.95.

Drag Divergence for Modified UAVs

The studies show that as far as Mdd is concerned,  a cost effective airfoil modification option can be used to increase the efficiency of a drone aircraft near Mdd and it can be effective as swept wings.  In addition, this aircraft can also be more efficient at lower speeds.

This is an example of valuable information than can be quickly obtained due to the unique algorithm contained in Stallion 3D.  The software can be used to compute lift, drag, moments and stability derivatives for your unique aircraft shape at subsonic, transonic and supersonic speeds.  Grid generation is automatic and the setup of a complete aircraft configuration can take less than one minute.

How would you use Stallion 3D to quickly solve your  aircraft modification problems?

For more information, please visit http://www.hanleyinnovation.com/ or call us at (352) 240-3658.

Save $2,500 on the perpetual license of Stallion 3D this month at the special price of $4,995 (instead of $7,495).  Please visit http://www.hanleyinnovations.com/stallion3d.html for details.  

Thanks for reading. 


Wednesday, May 9, 2012

Stallion 3D Comes to The Aerodynamics ClassPack

Every student in your class (or member of your small business group) can have a copy of the Aerodynamics ClassPack on their notebook computer for the entire year!

ClassPack is a yearly class/group license of our software suite consisting of  Stallion 3D, MultiSurface Aerodynamics, MultiElement Airfoils and VisualFoil Plus. Each module in ClassPack has proven accuracy and utility in both the professional and academic worlds.


The advantages of ClassPack include:
  • engaging content for lectures and labs
  • independent student activities
  • complete software packages (no need to purchase extra pre & post processing tools)
  • engineers and students do not need to have advanced aerodynamics or computer programming skills
  • accurate solvers for realistic project and lab experiments
  • interactive visualizations for engaging aerodynamics presentations and lectures
  • standard graphs (as you will find in text books or reports) & analysis for reports and capstone year end projects
  • design interface for international design competitions
  • ideally suited for fulfillment of design credits
  • already used in industry for aerodynamics conceptual analysis & design
Under the ClassPack license, all engineers, faculty, staff & students involved with a specific small business group or academic class will be able to access the software suite under a single class password.
The software can be installed in the classroom,  engineer or faculty offices, group members and students' PCs or notebooks and in labs associated with the class.


Stallion 3D race car simulation. Graph show surface velocity in m/s.

The Aerodynamics ClassPack Suite is ideally suited for:
  • aerodynamics conceptual analysis and design
  • introductory courses in aerodynamics and fluid dynamics
  • intermediate courses covering flow fields, airfoil analysis, 3D wing analysis & design, compressible flows & boundary layers and high lift devices
  • advanced courses covering 2-D panel methods, 3-D vortex lattice methods and finite volume CFD methods
  • senior projects & design-build-test competitions
  • consulting projects
  • aircraft, marine and automobile design and analysis
  • transonic and supersonic aircraft design and analysis

Stallion 3D Simulation of NASA CRM, 800K+ cells, 5% error in Cl/Cd (Cl=0.58).

The following modules are available in our class pack:
The introductory price for one year of the Aerodynamics ClassPack is $2,995.  Please click here to purchase.

For more information, please visit http://www.hanleyinnovations.com/classpack.html or call us at (352) 240-3658.
Please visit our YouTube channel at: http://www.youtube.com/user/hanleyinnovations?feature=guide

Tuesday, April 24, 2012

Setup Complete Aircraft for Analysis in About One Minute

Often it is necessary to analyze a complete airplane to determine loads, moments and stability (with and without stores, gears and external tanks) for various flight configurations.

Stallion 3D is a unique MS Windows software that simplifies this task by importing a CAD model that represents the geometry of interest and then automatically perform the necessary computing to generate the aerodynamics information.

Stallion 3D uses an novel formulation of the immersed boundary method, IBM, (based on a 3D Cartesian grid) to automatically detect immersed geometries and perform grid refinement at the boundaries.  Hanley's original ghost-cells based boundary scheme is automatic and can even work with near-zero-thickness surfaces to model sails and other aerodynamic structures.

The following video shows how to input the full 3D aircraft for analysis in Stallion 3D. Given a .stl (from NASA VSP, for example) the setup time is about one minute. Please click the following link to view the video:




More information about Stallion 3D can be found at: http://www.hanleyinnovations.com/stallion3d.html

Do not hesitate to contact us at (352) 240-3658 for more information.

BTW, here are a few recent pictures from Stallion 3D.  In some images, the geometries are from TurboSquid.com. Other geometries were created using Stallion's built-in wing editor.

Meteor at Mach 10.  Picture shows the temperature field.

Cartesian grid for joined-wing (box wing) model.

Sailboat simulation demostrating the ability to analyze thin surfaces.

Building and trees in the wind (steady flow).


Thanks for reading and best regards.

Wednesday, April 11, 2012

NASA Vehicle Sketch Pad

NASA's  Vehicle Sketch Pad (VSP) was released in January 2012 as an open source program.  VSP is an easy-to-use CAD software package dedicated to the rapid design of 3-dimensional solid models of airplanes, UAVs and other aircraft types.  More information about VSP (OpenVSP) and links to download a free copy can be found at the following page: http://www.openvsp.org.  The following video demonstrates the ease of use of VSP:


Additional tutorial information can be found at the following link:  http://www.openvsp.org/vid_tutorial.html

VSP exports to a variety of formats including .stl files.  This allows you to export your solid model for additive manufacturing or analysis in Stallion 3D and  other CAE programs:


Vehicle Sketch Pad and Stallion 3D (or similar program) are ideal tools for rapid aerodynamics conceptual design and analysis of aircraft.  Stallion 3D  can import the aircraft geometry in a single step using the .STL import function under the Design menu:

It's easy to import a STL file from VSP into Stallion 3D

Once the aircraft is imported in Stallion 3D, it will generate a grid and analyze the aircraft with a single click.  The user can also select the speed and other parameter for the aircraft.  In the following case for the Boeing 747-400, the speed is 290 meters/second and the angle of attack is 5 degrees:

This analysis shows the surface pressure and the Cp at various span locations.

Once you design and analyze one vehicle in VSP and Stallion 3D, it is hard to stop.  The following pictures show the pressure on the surface of two of the other complete aircraft that comes with VSP:

Pressure on surface of Cirrus aircraft included in VSP.

Pressure on the surface of  Cessna aircraft included in VSP

In short, NASA Vehicle Sketch Pad is a fun program to download and design aircraft.  It is even more fun to use Stallion 3D to analyze the aircraft and test the design in a digital wind tunnel.

More information can be found at http://www.hanleyinnovations.com/stallion3d.html
What is your favorite tools for rapid design and analysis?

Do not hesitate to email or call me at (352) 240-3658 if you have any questions. Thanks for reading and best wishes.  Patrick.

Friday, March 9, 2012

Replacing Paper: Future of Back-of-the-Envelope Analysis

Will the computer replace paper for rapid conceptual design & analysis?

Back in the day, if someone asked you a "quick" question or you had a brilliant idea (perhaps one that would change the world), the first thing to do is to move objects around your desk until you find a pencil and a piece of paper (the thought is fleeting and you will not remember if not immediately committed to paper).

Next, you feverishly sketch drawings and write down equations until you realize "ah, this will work! (or not)". This activity is the beginning of the conceptual analysis process. If your idea is really-really good, the piece of paper that you will randomly find is an envelope (perhaps from a bill or unsolicited advertisement).

The reason for the back-of-the-envelope calculation is to jot down your ideas using a medium that is totally familiar (and responsive) before you forget (or misinterpret) the volatile thought.

No matter how well you can draw or how quickly you can perform algebra, the back-of-the-envelope lacks robust computation power. It is often tucked into an ajar desk draw or between the pages of your favourite fluid dynamics text until you can find more time to complete the thought.

However, while we were sharpening our pencils, someone was trying to "improve" the back of the envelope process. The video below shows how a computer can be used to sketch drawings on a surface and the "paper" will actually solve the problem.



This can work for aerodynamics as well. The video below shows Hanley Innovations' MultiElement Airfoils as a conceptual analysis tool for deciding the position and orientation of a group of airfoils. The software can generate the lift, drag and moments for any configuration. It can save the configurations and export the shapes and positions to a .dxf file. More information can be found at http://www.hanleyinnovations.com/mefoil.html.




Paper is indeed changing. The video below shows Autodesk ForceEffect on the iPad. The program allows drawing on the screen to solve statics problem using free body diagrams.




Do you think that the computer will replace the back of the envelope?

For more information about Hanley Innovations' interactive aerodynamics analysis software, please visit: http://www.hanleyinnovations.com/

Thanks for reading, Patrick.