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Found one item.
  • Effects of the Propeller Advance Ratio on Delta Wing UAV Leading Edge Vortex

    K. A. Kasim, P. Segard, S. Mat, S. Mansor, M. N. Dahalan, N. A. R N. Mohd, M. N. M. Nasir
    6958-6970
    2019-10-03
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Indexed by:

2.27
2017CiteScore
 
 
82nd percentile - Automotive Engineering
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2.27
2017CiteScore
 
 
80th percentile - Mechanical Engineering
Powered by  Scopus

 

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IJAME | ISSN: 2229-8649 (Print); 2180-1606 (Online)
Automotive Engineering Centre
Universiti Malaysia Pahang Al-Sultan Abdullah
26600 Pekan, Pahang, MALAYSIA

© Universiti Malaysia Pahang Al-Sultan Abdullah Publishing

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