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Motion Optimistion Of Plunging Airfoil Using Swarm Algorithm

Electronic Theses of Indian Institute of Science

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Title Motion Optimistion Of Plunging Airfoil Using Swarm Algorithm
 
Creator Arjun, B S
 
Subject Airframes - Swarm Algorithms
Aerodynamics - Swarm Algorithms
Plunging Aifoils - Motion Optimisation
Particle Swarm Optimisation (PSO)
Non Uniform Rational Bezier Splines (NURBS)
Unsteady Flow Solver
Aeronautics
 
Description Micro Aerial Vehicles (MAVs) are battery operated, remote controlled miniature flying vehicles. MAVs are required in military missions, traffic management, hostage situation surveillance, sensing, spying, scientific, rescue, police
and mapping applications. The essential characteristics required for MAVs are:
light weight, maneuverability, ease of launch in variety of conditions, ability to
operate in very hostile environments, stealth capabilities and small size. There
are three main classes of MAVs : fixed, rotary and flapping wing MAV’s. There
are some MAVs which are combinations of these main classes. Each class has
its own advantage and disadvantage. Different scenarios may call for different
types of MAV. Amongst the various classes, flapping wing class of MAVs offer
the required potential for miniaturisation and maneuverability, necessitating the
need to understand flapping wing flight.
In the case of flapping winged flight, the thrust required for the vehicle flight
is obtained due to the flapping of the wing. Hence for efficient flapping flight,
optimising the flap motion is necessary. In this thesis work, an algorithm for
motion optimisation of plunging airfoils is developed in a parallel framework.
An evolutionary optimisation algorithm, PSO (Particle Swarm Optimisation),
is coupled with an unsteady flow solver to develop a generic motion optimisation
tool for plunging airfoils. All the unsteady flow computations in this work are
done with the HIFUN1 code, developed in–house in the Computational Aerodynamics Laboratory, IISc. This code is a cell centered finite volume compressible
flow solver. The motion optimisation algorithm involves starting with a population of motion curves from which an optimal curve is evolved. Parametric
representation of curves using NURBS is used for efficient handling of the motion
paths. In the present case, the motion paths of a plunging NACA 0012 airfoil is
optimised to give maximum flight efficiency for both inviscid and laminar cases.
Also, the present analysis considers all practically achievable plunge paths, si-
nusoidal and non–sinusoidal, with varying plunge amplitudes and slopes. The
results show promise, and indicate that the algorithm can be extended to more
realistic three dimension motion optimisation studies.
 
Contributor Balakrishnan, N
 
Date 2010-06-03T08:10:29Z
2010-06-03T08:10:29Z
2010-06-03
2008-09
 
Type Thesis
 
Identifier http://hdl.handle.net/2005/708
 
Language en_US
 
Relation G22948