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I was just wondering if this is a simmilar process that ED use to create their AFM for the SU-25 and KA-50?

 

http://www.dsto.defence.gov.au/publications/2256/DSTO-TR-0988.pdf

 

and if so can they do the P/C-9A as this would help me out alot :)

 

P.S. DSTO have alot of excelent quality data on offer pubilcy in terms of journal artilces if that can be utalised for Lockon so rather than the community finding some obsqure avionics article (for the F/A-18 :smilewink: ) that may like to concentrate on finding accurate and viable flight data.

 

If ED could respond that would be great as Iam interested in the simulation process and iam sure other people are also.

 

Cheeres

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Airplane Aerodynamincs and Performance

 

Airplane Aerodynamincs and Performance

 

AirplaneAeroAndPerformance.jpg

 

by Dr. Jan Roskam and Dr. Chuan-Tau Edward Lan

 

published by Design, Analysis and Research Cooperation

 

ISBN 1-884885-44-6

 

They should (if not already done) read things like that.

 

I have it and it rocks if u want to know something bout this topic.

[sIGPIC][/sIGPIC]

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Nice, will check it out.

 

I have "Aerodynamics for Engineers" by Bertin

 

http://www.amazon.com/Aerodynamics-Engineers-4th-John-Bertin/dp/0130646334

 

I got it for my 18th (yes its sad i know) and its great, not so great if you dont understand or want to understand vector calculus... but thats like everything in life ;)

 

I was more wondering on how ED implement aircraft measurements into a functioning model and which variables are of most importance?

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