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Phase II Final Report - NASA's Institute for Advanced Concepts

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Planetary Exploration Using Biomimetics<br />

An Entomopter <strong>for</strong> Flight on Mars<br />

80<br />

80<br />

60<br />

60<br />

40<br />

40<br />

Maximum<br />

Maximum Flap<br />

Flap Angle<br />

Angle 85°<br />

85°<br />

Flapping<br />

Flapping Frequency<br />

Frequency 4.43<br />

4.43 Hz<br />

Hz<br />

Excess<br />

Excess Mass<br />

Mass Capacity<br />

Capacity 1.5<br />

1.5 kg<br />

kg<br />

Wing<br />

Wing Length<br />

Length 0.6<br />

0.6 m<br />

Flight<br />

Flight Velocity<br />

Velocity 14<br />

14 m/s<br />

m/s<br />

20<br />

20<br />

0<br />

-20<br />

-20<br />

0.07 0.15 0.22 0.30 0.37 0.45 0.52 0.60 0.67 0.75 0.82 0.90 0.97<br />

0.07 0.15 0.22 0.30 0.37 0.45 0.52 0.60 0.67 0.75 0.82 0.90 0.97<br />

0.1<br />

r = 0.1<br />

0.2<br />

r = 0.2<br />

0.3<br />

r = 0.3<br />

0.4<br />

r = 0.4<br />

0.5<br />

r = 0.5<br />

0.6<br />

r = 0.6<br />

-40<br />

-40<br />

-60<br />

-60<br />

-80<br />

-80<br />

Wing Flap Cycle<br />

Wing Flap Cycle<br />

Figure 3-107: Angle of Attack <strong>for</strong> a Maximum Flap Angle of 85 o and Flight Speed of<br />

14 m/s<br />

3.3.3 Analytical Analysis of Mars Entomopter Aerodynamics<br />

3.3.3.1 Introduction<br />

The aerodynamic analysis of the Entomopter <strong>for</strong> the Mars exploration should be able to take into<br />

account the complete mission profile of Entomopter in the Mars environment. The optimal<br />

design should satisfy the lift and thrust requirements over the entire flight regime. In order to<br />

assess the per<strong>for</strong>mance of an Entomopter designed <strong>for</strong> Mars, it must first be proved that flapping<br />

wing chosen <strong>for</strong> its low speed flight capability, provides enough lift and thrust to make the Entomopter<br />

fly robustly. This requires an analytical model that gives satisfactory estimates <strong>for</strong> lift<br />

and thrust values <strong>for</strong> different flight conditions. The mission includes different phases of flight<br />

(takeoff, steady level flight, turning per<strong>for</strong>mance, maneuvers, and landing) that must be analyzed<br />

in depth <strong>for</strong> if accurate per<strong>for</strong>mance predictions are to be obtained. As a first step, only<br />

steady level flight has been considered, because that constitutes the major part of the mission.<br />

Another important requirement is the validation of the analytical results against corroborating<br />

results derived from CFD and ultimately experimental tests in a wind tunnel.<br />

Even though flapping wing flight is the major mode of locomotion used by birds and insects, no<br />

analytical model available has so far has been able to estimate the true per<strong>for</strong>mance of birds and<br />

insects. Many have studied flapping wing locomotion, but the complex modes of flight in nature<br />

still need to be addressed in much more detail and it will be some time be<strong>for</strong>e these complex<br />

motions and phenomena are completely understood. Based on prior work conducted by different<br />

researchers in this area, and taking into account the peculiar design of Entomopter, a physics<br />

116<br />

<strong>Phase</strong> <strong>II</strong> <strong>Final</strong> <strong>Report</strong>

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