DTIC ADA428842: Mini UAV’s: Can Active Flow pdf

DTIC ADA428842: Mini UAV’s: Can Active Flow

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Description of the Book:

What is All? 1) Eliminate low Re effects on performance; 2) Control attitudes and provide guidance; 3) Propulsion by periodic excitation; 4) No moving parts

• Creator/s: Defense Technical Information Center
• Date: 11/5/2002
• Year: 2002
• Book Topics/Themes: DTIC Archive, Seifert, Avi, TEL-AVIV UNIV (ISRAEL) DEPT OF FLUID MECHANICS AND HEAT TRANSFER, *EXCITATION, *DRONES, *MINIATURIZATION, *FLUID FLOW, PITCH(INCLINATION), MOMENTS, VORTICES, AIRFOILS, PIEZOELECTRIC MATERIALS, GUIDANCE, ACTUATORS, ANGLE OF INCIDENCE, THRUST VECTOR CONTROL SYSTEMS, DELTA WINGS, REYNOLDS NUMBER, WORKSHOPS, CLOSED LOOP SYSTEMS, ATTITUDE(INCLINATION), CONTROL JETS

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