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digital_datcom · Digital DATCOM Users

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Group Information

  • Members: 433
  • Category: Aerospace
  • Founded: Mar 3, 2006
  • Language: English
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Description

This group has been created to promote understanding of the USAF Digital DATCOM software package.

The Digital DATCOM is a large software tool set primarily used to estimate stability and control derivatives for an aircraft design. DATCOM takes its input from a text-based description of the aircraft's geometry.

Binaries, source code and sample input files for the Digital DATCOM are available for download from the Air Force Research Labs web site:

http://www.va.afrl.af.mil/org/VAC/VACA/vaca_index.html

Most Recent Messages

  (View All)
Re: Missile Simulator
This group deals with the Airplane Datcom only. The Missile Datcom is not publically available. You will have to pursue your requirements outside of this
Posted - Wed May 22, 2013 3:21 pm
Bill Galbraith
billgalbraith
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Missile Simulator
I am writing Missile simulator using MATLAB with following requirements 1. Multi-stage( upto 3 levels) Missiles 2. Generic Missile geometry user interface.
Posted - Wed May 22, 2013 2:28 pm
Naganna G e
naganna.ge
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Re: influence of swept angle on flying wing
No, I have done no work on your flying wing. The comparison was with my TSR2 model. I now have a reasonable match between Datcom, Panukl and a very small
Posted - Thu May 2, 2013 8:50 pm
Alan Teeder
ajtaa
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Re: influence of swept angle on flying wing
If other tools are giving you decent answers and Datcom isn’t, maybe the airplane isn’t the problem, maybe it’s the tools. Datcom might not be able to
Posted - Thu May 2, 2013 8:32 pm
Bill Galbraith
billgalbraith
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Re: influence of swept angle on flying wing
Hello Bill, Thank you very much indeed for the time you spent on this case. There is probably an intrinsic problem in my design and you have convinced me to
Posted - Thu May 2, 2013 8:27 pm
fredolegrand
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Message History

Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec
2013 21 6 31 28 9
2012 17 7 2 12 9 10 14 1 5 6 33
2011 17 41 59 34 35 18 6 15 4 12 2
2010 33 46 46 40 23 28 34 4 27 10 20 35
2009 32 26 54 49 5 4 12 34 10 41 29 7
2008 32 35 14 13 6 13 5 6 22 10 28 3
2007 10 18 3 55 8 37 30 6 23
2006 6 5

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