A numerical prediction and flight test of the transient fuel temperatures in an aircraft-Reference-Cited by-同舟云学术

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A numerical prediction and flight test of the transient fuel temperatures in an aircraft

Published:2007-12 Issue:12 Volume:21 Page:2250-2260
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Kim Yeong Jun,Kim Chang Nyung

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/BF03177487.pdf

Reference12 articles.

1. I. Moir, and A. Seabridge, Aircraft Systems: Mechanical Electrical, and Avionics Subsystem Integration,AIAA 17, (2001) 35–182.

2. K. Huenecke, Modern Combat Aircraft Design, Naval Institute Press, MD, USA, (1987) 23–28.

3. Network Analysis Inc., SINDA/G Library Reference Guide, Network Analysis Inc., AZ, USA, (1996) 39–40.

4. Network Analysis Inc., SINDA/G User’s Guide, Network Analysis Inc., AZ, USA (1996) 39–40.

5. NATO Code Number O-156;DoD,1997

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