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Steady-State/Transient Performance Simulation of the Propulsion System for the Canard Rotor Wing UAV During Flight Mode Transition.

Author(s):
Publication title:
A.S.M.E. paper
Title of ser.:
ASME Technical Paper : GT
Ser. no.:
2004
Pub. Year:
2004
No.:
GT2004-53739
Paper no.:
GT2004-53739
Pages:
9
Pub. info.:
New York, NY: American Society of Mechanical Engineers
Language:
English
Call no.:
A11800
Type:
Technical Paper

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