Analysis of UAV wing using composite structure
Title
: 
Analysis of UAV wing using composite structure

Personal Author
: 
Wong, Zi Jing

Publication Information
: 
Skudai : Universiti Teknologi Malaysia, 2005

Physical Description
: 
1 CD-ROM ; 12 cm.

General Note
: 
Also available in printed version : TL699.C57 W66 2005 raf

Subject Term
: 
Airplanes -- Materials
 
Airplanes -- Wings -- Mathematical models
 
Composite materials -- Mechanical properties -- Mathematical models
 
Finite element method

Project Paper (Sarjana Muda Kejuruteraan (Mekanikal - Aeronautik)) - Universiti Teknologi Malaysia, 2005


LibraryItem BarcodeCall NumberMaterial TypeItem Category 1
FKM LibraryFKM30000002765CP 8939Computer File Accompanies UTM Thesis/Project PaperCompact Disc Accompanies UTM Thesis/Project Paper
PSZ JB30000010092128CP 8939UTM Special Collection - Computer FileCompact Disc Accompanies UTM Thesis/Project Paper