|
| If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|||||||
|
|
Thread Tools | Display Modes |
|
|
|
#1
December 7th 09, 10:21 PM
posted to rec.aviation.homebuilt
|
|||
|
|||
NACA profile calculations
jan olieslagers wrote:
And also, less poignant but still: How do I calculate from the basic parameters the behaviour of the profile, i.e. the Cl curves? And perhaps other nice info like the leading edge diameter? Generally: any pointers to in-depth information that a non-engineer can mentally digest? Have you checked out some of the links at CFD Online: http://www.cfd-online.com/ In particular, they have links to various software around the web: http://www.cfd-online.com/Links/ 
|
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Calculations for Flying | javawizard | Piloting | 11 | October 18th 07 05:22 PM |
| NACA Numbers??? | c hinds | Home Built | 3 | October 11th 04 09:40 PM |
| NACA Chord Balance point | [email protected] | Rotorcraft | 3 | April 27th 04 06:05 AM |
| Reverse NACA duct | Chris W | Home Built | 22 | October 28th 03 10:59 PM |
| NACA duct ventrui | Chris W | Home Built | 7 | October 27th 03 04:11 PM |
Hybrid Mode
