AERODYNAMIC STABILITY AND MANEUVERABILITY OF THE GLIDING FROG POLYPEDATES DENNYSI
University of California Berkeley, Department of Integrative
Biology, Berkeley, CA 94720-3140, USA
*
e-mail:
mccay{at}socrates.berkeley.edu
Accepted May 29, 2001
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Summary |
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Key words: gliding, maneuverability, aerodynamic stability, Polypedates dennysi, tree frog
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Introduction |
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Gliding frogs
Gliding originated independently within two families of tree frogs, the
Hylidae and the Rhacophoridae (Emerson and Koehl,
1990). Within each evolutionary
lineage are extant species spanning the full range of gliding abilities:
non-gliding species, intermediate species and gliding species (Duellman,
1970
; Emerson and Koehl,
1990
). Therefore, tree frogs
present an excellent system in which to study the origin of gliding because
they are living, behaving organisms that possess a range of gliding abilities
that can be directly observed and compared.
Gliding tree frogs of both families share a suite of morphological features
(e.g. enlarged, extensively webbed hands and feet, skin flaps on elbows and
ankles) and use similar limb postures while gliding (Emerson and Koehl,
1990; M. G. McCay, personal
observations). These frogs use gliding to descend from the canopy down to
mating sites over temporary pools on the rainforest floor (Roberts,
1994
) and to escape from
predators (Emmons and Gentry,
1983
). Emerson et al. (Emerson
et al., 1990
) compared the
gliding performance of gliding frogs with that of non-gliding frogs and found
that the morphological features and limb postures of the gliding frogs were
associated with higher gliding distances and much greater maneuverability.
Aerodynamic stability and maneuverability
Animal flight is a complex interaction between aerodynamic forces and
torques, the animal's mass properties and the behavior of the animal. The
motion an animal experiences during flight is marked by transitory
oscillations (phugoid mode, short-period mode, Dutch-roll mode and spiral
mode) superimposed over translation along a flight path (McCormick,
1976). In addition, the flight
path may be changing as a result of postural changes by the animal.
Maneuverability is the ability of a gliding animal to accelerate and change its flight path. In general, a gliding animal is capable of accelerating linearly (such as slowing down) and rotationally (such as twisting around the cranialcaudal axis). Here, I will examine turning, or changing the animal's direction of gliding. Turning maneuvers are accomplished by rotations about the glider's center of mass that in turn alter the aerodynamic forces acting on the glider. This rotation can be resolved into rotations about three orthogonal axes, pitch, roll and yaw, as shown in Fig. 1. Maneuverability depends on the magnitude of the aerodynamic forces the frog can generate as well as the frog's aerodynamic stability.
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Aerodynamic stability is the ability of a gliding animal to maintain its flight path in the presence of perturbations. When perturbed from some initial position, a gliding animal that is aerodynamically stable will return passively to its original position, much like a weathervane aligns itself passively with the wind. Thus, aerodynamic stability is a passive interaction between a gliding animal's morphology and the surrounding airstream that allows an animal to maintain its direction of flight without actively steering to control its direction of flight.
A gliding animal experiences many transitory oscillations in the course of
gliding. If an animal is dynamically stable, these oscillations will damp out
in the absence of any behavioral control on the part of the animal. If the
animal is dynamically unstable, these oscillations will grow in magnitude
unless the animal actively steers to counteract the oscillations. Dynamic
stability depends on both the mass properties of the animal and its
aerodynamic properties, including aerodynamic stability (McCormick,
1976). The more
aerodynamically stable a gliding animal is, the more likely that the animal
will be dynamically stable (McCormick,
1976
).
Aerodynamic stability can be quantified as the change in aerodynamic torque
per unit rotation about an axis (i.e. the slope of the graph of aerodynamic
torque plotted as a function of rotation angle) (McCormick,
1976).
Fig. 2 shows a hypothetical
plot of the change in pitching torque as a function of angle of attack for a
stable frog (Fig. 2A), a
neutrally stable frog (Fig. 2B)
and an unstable frog (Fig. 2C).
A linear regression through the pitching torque data as a function of angle of
attack is used to assess the stability of the frog about its pitch axis. The
examples shown in Fig. 2
intersect the horizontal axis (angle of attack) at the equilibrium point, the
angle at which no aerodynamic torque acts to rotate the frog; the frog
naturally glides at the angle of attack corresponding to the equilibrium
point.
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In Fig. 2A, if the frog's angle of attack is perturbed in a nose-up direction, an aerodynamic torque is induced that rotates the frog in a nose-down direction, back towards equilibrium. If the frog is perturbed in a nose-down direction, an aerodynamic torque is induced that rotates the frog nose-up, back towards equilibrium. A frog with these aerodynamic characteristics is aerodynamically stable.
The slope of the linear regression of aerodynamic torque about the pitch axis versus angle of attack determines the level of aerodynamic stability that the frog possesses about the pitch axis. A steep negative slope indicates that a large restoring torque would be induced for a small change in angle, so the frog would be highly stable. A flatter negative slope indicates weaker stability because a smaller restoring torque would be induced for a change in angle. Zero slope (a horizontal line) (Fig. 2B) indicates neutral stability because torque would not change with angle, no restoring torque would be induced and the frog would remain at the angle to which it was perturbed. A positive slope (Fig. 2C) indicates an unstable frog, since any perturbation in angle of attack away from the equilibrium point induces a torque that would rotate the frog further away from the equilibrium point.
A potential trade-off exists between aerodynamic stability and
maneuverability (Maynard Smith,
1952); aerodynamic stability
minimizes the effect of random perturbations (such as wind gusts), but
aerodynamic stability also counteracts intentional perturbations performed by
the animal (such as the initiation of turns). A gliding animal that is
aerodynamically stable has a more sluggish initial response to a steering
motion than does a gliding animal that is aerodynamically unstable. Therefore,
an aerodynamically stable frog must execute a steering motion much more
forcefully to accomplish the same maneuver in the same amount of time as an
aerodynamically unstable frog. However, a gliding animal that is
aerodynamically unstable requires more active steering to maintain its
direction of flight than does an animal that is aerodynamically stable because
each wind gust that hits the animal causes it to veer off course unless the
animal actively executes a steering motion to get itself back on course.
Thus, if a gliding frog is airborne and a wind gust disturbs the animal from its intended path, the animal can regain its original flight path in one of two ways: (i) it can change its posture and actively steer itself back on course, or (ii) if the frog is aerodynamically stable, it can remain in the same fixed posture and let its aerodynamic stability return it back on course. The presence or absence of aerodynamic stability directly affects the amount of corrective steering required to glide successfully.
Although aerodynamic stability and maneuverability are central issues in
animal flight, few investigators have actually measured the aerodynamic
stability and maneuverability of animals (Harris,
1936). Once stability and
maneuverability have been measured, meaningful assessments of the trade-off
between stability and maneuverability can be made. In addition, once stability
and maneuverability have been well characterized, assessments of the
behavioral control of flight may also be performed. However, before assessing
the trade-off between stability and maneuverability, one must first understand
the basic physical mechanisms used by tree frogs to glide and maneuver.
Objectives
The purpose of this study was to determine how tree frogs glide and
maneuver by observing the behavior of live gliding tree frogs. The specific
questions addressed were as follows. (i) What physical mechanisms do gliding
frogs use to accomplish maneuvers? (ii) Are gliding frogs aerodynamically
stable or unstable? (iii) How maneuverable are gliding frogs compared with
other gliding animals? A thorough understanding of the aerodynamic issues
associated with gliding provides a solid foundation from which to investigate
the evolution of gliding in tree frogs.
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Materials and methods |
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Maneuvers with a stimulus
Gliding conditions were simulated using a tilted wind-tunnel similar in
design to tilted wind-tunnels used previously to study the flight of birds
(Pennycuick, 1968; Tucker and
Heine, 1990
). When a frog
glides through the air, the airflow with respect to the frog is parallel to
the frog's flight path, but in the opposite direction from that in which the
frog is moving (see Fig. 3A).
The airflow past a frog that is gliding in the working section of the tilted
wind-tunnel simulates the airflow relative to a frog gliding through still air
(see Fig. 3B). Tree frogs glide
through the air on an inclined path; the angle that the frog's glide path
makes with respect to the ground is the frog's glide angle (see
Fig. 3A). In addition, a
gliding frog's entire body is inclined relative to its glide path; the angle
between the frog's body (snout-to-vent line) and its glide path is the frog's
angle of attack (see Fig.
3A).
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A glide angle of 45° was used in the tilted wind-tunnel in this study, corresponding to glide angles observed from videotaped glides of frogs in open air filmed in the laboratory. Airspeeds were set to a level (between 12 and 14 m s-1) that suspended the frogs in the tunnel's airflow with no rising or falling movement; this airspeed range corresponded to a Reynolds number range from 75 000 to 100 000 for the frogs. Larger, heavier frogs required higher airspeeds (14 m s-1) to generate the higher aerodynamic forces required to simulate gliding in open air. All wind-tunnel runs were performed at room temperature (24-27°C).
The tilted wind-tunnel used for these experiments had a transparent Plexiglas test section through which the frogs were videotaped. Airspeed was controlled using a variable-resistance rheostat (Powerstat type 3PN116, The Superior Electric Company, Bristol, CT, USA) that controlled airspeed over the range 0-18 m s-1. The wind-tunnel had a contraction ratio of 3.4 and a turbulence intensity of less than 1 % over the full range of tunnel speeds, as measured using a hot-wire anemometer (Kurz air velocity meter, model 443M). The test section had a safety net installed to prevent accidental movement of a frog into the expansion chamber of the wind-tunnel.
The stimulus used to induce a frog to turn was a plastic plant similar to plastic plants kept in each frog's living quarters. The plant was stuck to the outside of the wind-tunnel test section so that it was visible to the frog but did not change the airflow within the test section. The stimulus treatments used were (i) no plant (control), (ii) plant on the left side of the test section, and (iii) plant on the right side of the test section. Each frog was exposed to each of the stimulus treatments 20 times. All treatments for all frogs were used on each of two days, with the order of individual frogs and treatments determined using a random number table.
During a wind-tunnel run, the plant stimulus was put into place, and the frog was removed from its container and released into the tunnel test section. The frog was released at an angle of attack of approximately 45°, with its mid-sagittal plane parallel with the direction of airflow (i.e. zero yaw angle). The frog's motion and behavior during each wind-tunnel run were videotaped from above and from the side (see Fig. 3B) using video camcorders (Sony Hi-8 video camera recorders CCD-V9 and CCD-TR101) at a rate of 60 frames s-1.
The videotaped wind-tunnel runs were examined to determine maneuvering behavior. A run was scored as a turning maneuver if the frog's final snout orientation had changed in yaw angle by more than 60°. Maneuvers were scored as (i) left turn, (ii) no turn or (iii) right turn.
Posture during maneuvers
Videotapes from the wind-tunnel runs described above were analyzed to
identify changes in the frog's posture while turning. The positions of a
frog's arms and legs were noted, and the movements of these limbs were
qualitatively determined in three directions: forwardaft
(cranialcaudal), towards and away from the center line of the body
(lateral), and above or below the plane of the body (dorsalventral).
Selected runs were analyzed in the Peak Motus 3-D motion-analysis system to
acquire the three-dimensional coordinates of the frog's appendages with
respect to its center of mass; the calculated coordinates were used to verify
the qualitative observations of limb postures from the selected runs. Limb
postures and motions qualitatively observed when frogs executed turns were
compared with those observed when frogs were gliding without turning to
identify behaviors that were potentially involved in maneuvering.
Three-dimensional kinematic analysis of turns
Wind-tunnel runs were identified from videotape where (i) the frog was
centered in the wind-tunnel test section with no yaw angle when first released
into the test section, and (ii) the frog moved from the center of the test
section to the test section wall on the frog's left or right. These videotaped
wind-tunnel runs were used in a three-dimensional motion analysis to determine
the frog's rotations while maneuvering. The videotapes were analyzed in the
Peak Motus 3-D motion-analysis system to acquire the three-dimensional
coordinates of the frog's body features throughout the course of a maneuver.
These three-dimensional coordinates were used to calculate the frog's rotation
about the pitch, yaw and roll axes during the course of a maneuver. Changes in
pitch and roll angles with respect to the horizontal plane and changes in yaw
angle with respect to the direction of airflow in the test section were
calculated. These angles were compared between wind-tunnel runs to determine
whether any differences in angular orientations during a turn were associated
with a particular posture.
Stability of gliding frogs
Torques acting on Polypedates dennysi were measured using a
full-scale physical model of the frog in the wind-tunnel. The model was
fabricated by making an impression of a preserved adult Polypedates
dennysi specimen in dental alginate (Jeltrate alginate impression
material, Dentsply International Inc.), then casting the frog model in
flexible silicone (LS-40 silicone rubber, BJB Enterprises, Inc.) with a rigid
wire skeleton inside. The frog model was posed in a fixed posture
corresponding to the posture used by the live gliding frogs in the tilted
wind-tunnel. The frog model was mounted on an instrumented balance that
measured the torque acting about the model's center of mass.
Torques were measured about the pitch axis at angles of attack of 0, 20, 30, 45, 60 and 90°. Each series from 0 to 90° was repeated five times. Similar series were run to measure torques about the roll axis and yaw axis for roll (and sideslip) angles of 90, 60, 45 and 30° to the left and 0, 30, 45, 60 and 90° to the right.
As described above, the slope of the linear regression of the aerodynamic
torque plotted as a function of rotation angle determines the aerodynamic
stability. To compare the aerodynamic stability of Polypedates
dennysi with that of other gliding animals, the effects of the frog's
physical size and airspeed must be removed from the stability slopes described
above. The effects of size and airspeed were removed from the stability slopes
by dividing these slopes by the frog's planform area (the projected area of
the frog as seen from above), its snoutvent length (the distance from
the tip of the frog's snout to its cloacal opening) and the dynamic pressure
(the portion of the total energy of a moving fluid due to kinetic energy)
(Vogel, 1994) at which the
torque data were measured in the wind-tunnel, yielding three dimensionless
stability coefficients (McCormick,
1976
).
The stability slopes were divided by snoutvent length, rather than wing chord length or wing span, because snoutvent length was an easily measured physical length of a frog that does not change when the frog assumes different postures. In addition, snoutvent length is of the same order of magnitude with respect to overall size as wing chord length and wing span, so the absolute values of the stability coefficients will be consistent with those of other animals and/or aircraft.
The stability coefficients defined below are analogous to the dimensionless
lift coefficient (CL) and drag coefficient
(CD) used in other fluid dynamic analyses (Vogel,
1994). The conventions and
notations used to define the stability coefficients are taken from aircraft
stability and control theory (McCormick,
1976
).
Rolling stability coefficient Cr,
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In engineering literature, wing span is used in place of in
equation 2. In addition, rolling moment has previously been assigned the
symbol L (McCormick,
1976
); I use the symbol
R to avoid confusion with aerodynamic lift, which also uses the
symbol L.
Pitching stability coefficient Cm,
Yawing stability coefficient Cn,
The sign of the slope of the measured torque versus angle will determine whether or not the frog is stable. Because the torque and angle are defined as positive in the same direction for pitch, roll and yaw, a negative stability coefficient indicates aerodynamic stability. A positive stability coefficient indicates aerodynamic instability, and a stability coefficient of zero indicates neutral stability.
Maneuverability of gliding frogs
Using aerodynamic forces measured from a full-scale physical model in the
wind-tunnel, the maneuverability of different turns can be compared. The same
physical model of Polypedates dennysi used to measure aerodynamic
torques above was used for the aerodynamic force measurements. The frog model
was mounted on a device that measured the aerodynamic force acting on the
model in a single direction, and force measurements were taken using a similar
protocol to the aerodynamic torque measurements described above.
Fig. 4 illustrates the
aerodynamic forces that describe the frog's ability to turn for two types of
turn: banked turns and crabbed turns. These two types of turn represent two
different turning strategies that utilize different physical mechanisms to
achieve a turn. In a banked turn (Fig.
4A), the frog rolls into the turn. The banking frog's lift force
vector is tilted towards the center of the turn because of the frog's roll
angle. The component of the lift force acting towards the center of the turn
is the centripetal force that pulls the frog through the turn. In a crabbed
turn (McCormick, 1976), the
frog yaws into the turn (Fig.
4B). By yawing, the frog induces a sideways-directed force that
acts towards the center of the turn. This force is the centripetal force that
pulls the frog through the turn.
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Lift force was measured at angles of attack of 0, 20, 30, 45, 60 and 90°, and centripetal force was measured at yaw angles of 0, 15 and 30° to the left and 15 and 30° to the right.
One way to quantify maneuverability is to assess how much centripetal
turning force can be generated for a given change in rotation angle. To
generate the centripetal force necessary to turn at a desired rate, how far
does one need to rotate? The higher the centripetal force per degree of
rotation, the more responsive the frog will be to rotations (banking or
yawing), and therefore the more maneuverable the frog will be. For crabbed
turns, the change in centripetal force Fc per change in
yaw angle (Fc/
) is given by the slope of
the linear regression through the measured centripetal force data (in the
engineering literature, `side force') plotted as a function of yaw angle. For
banked turns, the maximum turning force for a given roll angle is achieved at
the maximum lift force:
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The change in turning force per unit angle in a banked turn is given by:
To compare maneuverability between different animals, the effects of the
animal's weight must be removed from the slopes given agove
(Fc/
for crabbed turns,
Fc/
for banked turns). The slopes given
above divided by the animal's weight W yields a dimensionless index
of maneuverability (Im).
For crabbed turns:
For banked turns:
Results
Maneuvering mechanisms of gliding frogs
The frequencies of turning behaviors for each stimulus treatment (plant to
left, no plant or plant to right) for each frog are shown in
Fig. 5. The frequencies are
calculated as a percentage of the total turning behaviors observed for a given
stimulus treatment. The turning behavior of all three frogs changed
significantly in the presence of the plant stimulus, although the direction of
change was inconsistent between frogs. Frog 1 turned more away from the plant
stimulus, and frogs 2 and 3 turned more towards the plant stimulus. These data
demonstrate that P. dennysi does maneuver in response to the stimulus
provided.
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The frequencies of the frog's postures while turning to the left, going straight or turning right are shown in Fig. 6 for each of the three frogs. The frequencies are expressed as a percentage of the total observations of a given maneuver. All three frogs exhibit similar postures when turning, namely the foot opposite to the turn is held higher. For example, in a turn towards the left, the frog's right foot was held higher. However, for 35 % of the observed turns, the feet were held at equal heights. These two postures correspond to the two different turning techniques used by Polypedates dennysi.
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Pitch, roll and yaw angles during two turns to the left are shown in Fig. 7: a banked turn with the feet held at equal heights (Fig. 7A) and a crabbed turn with the right (opposite) foot held higher (Fig. 7B). Pitch angle is relatively constant and equal to approximately 60° for both turns shown. Yaw angle changes by the same magnitude (80°) at approximately the same rate (400° s-1) for both turns. However, roll angle differs between the two turns, covering approximately 60° for the banked turn and 0° for the crabbed turn.
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Aerodynamic stability of gliding frogs
The torques acting on a full-scale physical model of P. dennysi in
a wind-tunnel are shown in Fig.
8A-C. Stability coefficients are shown in
Fig. 8D. The frog is slightly
stable about the pitch and roll axes and is slightly unstable about the yaw
axis.
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Maneuverability of gliding frogs
The maneuverability index for the gliding frog performing a banked turn is
6.1x10-5 to 1.1x10-4rad-1 and for
a crabbed turn is 5.4x10-5 to
8.2x10-5rad-1. In contrast, the maneuverability
index calculated for a falcon Falco jugger from data in Tucker and
Parrott (Tucker and Parrott,
1970) is
1.8x10-4 to 3.3x10-4rad-1. The
maneuverability index for a banked turn is slightly higher than the
maneuverability index for a crabbed turn. Both the banked and crabbed turns of
the gliding frog have lower maneuverability than the maneuverability of a
falcon performing a banked turn.
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Discussion |
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The calculated maneuverability indices provide insight into the mechanical consequences of utilizing a banked turning technique as opposed to a crabbed turning technique. The maneuverability index of a frog using a banked turning technique is only slightly higher than that of a frog using a crabbed turning technique. This is because the frog's morphology produces only marginally more aerodynamic lift than centripetal force. In contrast, a falcon, with a morphology considerably better suited to produce aerodynamic lift, has a maneuverability index for banked turns that is as much as three times higher than that of a frog.
In addition, frogs and birds use gliding in very different ways. Birds
often glide while foraging, using thermals or wind currents to remain aloft
for extended periods with little metabolic energy expended for flight. Frogs
glide while travelling down from the canopy to mating sites on the forest
floor (Roberts, 1994) and to
escape predators (Stewart,
1985
; Scott and Starrett,
1974
). For birds, low-drag
flight is of importance since aerodynamic drag reduces the time aloft while
gliding. Frogs have not been observed actively decelerating prior to landing
(Roberts, 1994
), so minimizing
gliding speed by gliding with relatively high aerodynamic drag would reduce
the frog's impact speed when landing.
Much less additional aerodynamic drag is induced by turning using a banked
turn compared with turning using a crabbed turn (McCormick,
1976). Thus, for birds,
gliding using banked turns allows the bird to stay aloft longer because
aerodynamic drag is lower than if the bird turned using a crabbed turn. For
tree frogs, the potentially higher drag of crabbed turns will reduce gliding
speed and, thus, reduce landing impact speed.
Stability
As discussed above, the passive aerodynamic stability of an animal directly
affects the magnitude and rate of postural adjustments required to maintain a
desired glide path in the presence of random disturbances such as wind gusts,
but also adversely affects the maneuverability of the animal. Previous
investigators posited that an evolutionary lineage that develops the ability
to glide starts primitively as a glider that is passively stable and then
gradually loses passive aerodynamic stability as each successive species'
nervous system develops and refines the postural control necessary to
stabilize actively (Maynard-Smith,
1952; Caple et al.,
1983
). Implicit in this
hypothesis is the assumption that a stable glide path is an extremely
important aspect of gliding. Some investigators who have studied the
development of flight in lineages such as insects (Wootton and Ellington,
1991
) and bats (Norberg,
1985
) assume passively stable
gliding to be an initial step towards developing the ability to glide.
Because frogs as a group are known more for their jumping ability than for
their gliding ability, one would predict that gliding frogs should possess
strong passive aerodynamic stability. One possible reason that gliding tree
frogs are not highly stable is that the canopy environment through which frogs
glide may be relatively sheltered from winds (Monteith and Unsworth,
1990; Campbell,
1977
), so that tree frogs may
rarely encounter random disturbances to their direction of flight due to wind
gusts. Thus, aerodynamic stability may never have been of ecological
importance to gliding tree frogs.
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Acknowledgments |
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References |
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