You MUST be a MEMBER in Hip Pocket Aeronautics "Builders' Forum" to REGISTER for access to the Plan Gallery.
Forum Members can visit This Topic in the Forum to Register. Logging In to the Forum is required.
Home / Airfoils and Propellors and Aerodynamic Calculators / Source code. Tail Vol Coefficient, Static Margin &tc. Calculation of. Top Plans  New Items (Last 10 days)  Search  

Registered users

Username:

Password:

Log me on automatically next visit?

» Forgot password

 

Random Plan

Beta Major Be 250 (Plan and Article)
Beta Major Be 250 (Plan and Article) (hlsat)
Outdoor Power
Comments: 1
Downloads: 261

 


Source code. Tail Vol Coefficient, Static Margin &tc. Calculation of.
Source code.  Tail Vol Coefficient, Static Margin &tc. Calculation of.

             << ZIP may not work for everyone

Source code. Tail Vol Coefficient, Static Margin &tc. Calculation of.
Description: It's not an aerofoil nor a propellor, but this seems like the least unsuitable place for this.

C# (.Net Core 6) Source code to calculate Tail Volume Coefficient (Vh), Static Margin, Tail Moment arm and other odds & ends for a model. Derived (polite term for wholesale pilfering) from John Barker's (Hepcat, late of this Parish) spreadsheet.

This util also allows you to run the McCombs approximation for the model and, or apply a scaling factor to the tail area without having to edit the model's configuration file.

Content.

Source code (C#)
Example configuration files (.JSON)
Notes on use. (PDF)

The code should be fairly easy to port to other versions of the .Net framework or another language and development toolset entirely.

If you want to build the util as is you'll need to install .dotnet (Windows, Linux or Mac) and Visual Studio Code which are (as of April '23) free to download and use.

If you aren't a programmer and you'd like a version built for x64 Ubuntu/Debian Linux (built on Mint) send me a PM with your e-mail address and I'll send you the necessary files.
Keywords: John, Barker, Tail, Volume, Moment, Arm, Static, Margin, Coefficient, Vh, Hepcat, Lulu
Date: 04.06.2023 20:20
Hits: 476
Downloads: 109
Rating: 0.00 (0 Vote(s))
File size: 70.3 KB
Added by: TheLurker

Comment:
Sundance12
Admin

Join Date: 02.17.2008
Comments: 13
Heading Adjusted

Included Aerodynamic Calculators
04.07.2023 13:02 Offline Sundance12 shoelessbruce12 at gmail.com http://www.hippocketaeronautics.com



Previous Plan:
Single Blade Propellers  
 Next Plan:
SVG Aerofoils plus data files and source code to (re)create.

 

 

RSS Feed: Source code.  Tail Vol Coefficient, Static Margin &tc. Calculation of. (Comments)