Mechanical Desktop

Mechanical Desktop

4 Posts
0 Kudos
Registered: ‎05-10-2013
Post 1 of 1

parameterize a profiled blade using superposition of NACA profiles

457 Views, 0 Replies
05-10-2013 03:07 AM

Please, i want to modelize and parameterize a profiled blade using superposition of NACA profiles. 
To modelize and parameterize the profile of this blade using superposition of NACA profiles, i can import from Excel the points of the naca-profile direct in Inventor. But the problem is: I can not parametrize or change direct in Inventor the parameter of this curve. 
My challenge: i want to use a mathematical equation to generate the profile direct in Inventor. So i can select later the NACA-Model and select the preferred thickness, camber and camber location direct in Inventor to optimize the Blade. 
I don't need the coordinates of the airfoil/NACA-profile, but i want to generate it direct in Inventor.
Of course i want a program to set this NACA-Profil direct in Inventor. Probably use VBA-Code. 
Can you tell me please how i can use VBA to set any curve in Inventor? 
Do you know please, how i can use a mathematic equation to generate this point direct in Inventor? 
How do you modelize a profiled Blade using NACA-Profile? 
thank you verry much 

Best Regards

Post to the Community

Have questions about Autodesk products? Ask the community.

New Post
Manufacturing Community
The Manufacturing Community provides additional access to tips, tutorials, blogs and networking with peers.