Allometry of bat wings and legs and comparison with birds wings

Allometric equations on wing dimensions versus body mass are given for eight species of megabats and 76 species of microbats, on forearm length versus mass for 14 species of mega bats and 90 species of microbats, and on lower leg length versus mass for 11 species of megabats and 45 species of microbats. Megabats have, on average, shorter wing span, small wing area, higher wing loading and lower aspect ratio than have frugivorous microbats and the insectivorous vespertilionids of similar mass. Vespertilionids have the longest span, largest wing area and lowest wing loading in relation to body mass of the bat groups for which regression lines were calculated (megabats, frugivorous microbats, vespertilionids, molossids), characteristics that are important for slow flight and manoeuvrability for insect capture. Molossids have the highest wing loading of the groups. There is a weak tendency towards higher aspect ratio for larger bats than for smaller ones (positive slope). The slopes for most characters fit geometric similarity or have confidence intervals including the value for geometric similarity. Only in three cases does the slope lie nearer that for elastic similarity: for the forearm in nycterids and emballonurids and the lower leg length in molossids. Also in these cases the confidence intervals are wide and include the value for elastic similarity and that for geometric similarity as well. In megabats the slope for the lower leg length is much steeper than for geometric similarity. The slope for the forearm length is rather similar to that for wing span in the various groups. Megabats and frugivorous microbats have rather similar slopes for all the characters measured, but differ from the other groups only in wing area, wing loading and aspect ratio. The two frugivorous bat groups also have about the same elevation of the regression lines for aspect ratio and forearm length. Megabats and frugivorous microbats thus show a close convergence in wing area, wing loading, aspect ratio and forearm length. The regression equations provide ‘norms’ for the respective bat groups. Those species that deviate 10% or more from the mean trends for wing measurements are divided into different groups, based on the wing’s aspect ratio and loading. Bats with low aspect ratio wings usually have large pinnae, which improve the ability to discover small objects such as insects on leaves. Families or species of bats with wings of low aspect ratio are, for instance, Megadermatidae, Nycteridae, Rhinolophus ferrumequinum (Rhinolophidae), Chrotopterus auritus (Phyllostomidae) and Plecotus (Vespertilionidae). The group with average aspect ratio wings contains bats with different kinds of flight style and foraging behaviour, for instance many pteropodids, phyllostomids and vespertilionids. Bats with high aspect ratio wings are, for instance, Molossidae, Rhynchonycteris naso (Emballonuridae) and Nyctalus leisleri (Vespertilionidae). The regression lines for wing span, area and loading in megabats lie almost in the region of the lines for Greenewalt’s (1975) passeriform group, whereas the span and area for vespertilionid bats are larger and the wing loading much smaller than for most birds of similar mass. Molossid bats have a larger relative wing span and aspect ratio than have most birds, and a wing area and loading similar to those of small birds of the passeriform group. Vespertilionid bats have about the same aspect ratio as birds of the passeriform group, whereas megabats have somewhat lower ratios. Molossid bats show strong convergence with swifts and swallows in foraging behaviour and in wing form. Similar convergences can be found between various vespertilionid bats, flycatchers and swallows.

2021 ◽  
Author(s):  
Yukei Oyama

This undergraduate paper demonstrates the design, analysis, and manufacturing of a rocket deployable electric powered experimental unmanned aerial vehicle. The design process begins with defining the volume and dimensions of the allocated payload space for the UAV in the rocket. These dimensions are given by the aerostructures sub team in the Ryerson Rocketry Club. The dimensions given were used to determine the best configuration for the mission. The wing loading, power loading and endurance of the UAV are obtained from the constrained payload volume in the rocket and the avionics system of the of the UAV. The wing area, UAV weight and power requirements were calculated based on the previously determined values. The power requirement determines the motor size and propeller configuration. Aerodynamics, stability, and control were based the selected airfoil and obtained wing area. After completing the design, foam, additive manufacturing, and composite layups were used to create prototypes of the UAV. These prototypes were used to iterate the aircraft and address any immediate changes. The chosen design is a foldable flying wing, once deployed from the rocket has a wingspan of 70 inches, an aspect ratio of 13.35 and a surface area of 367 in2 . A prototype was created to prove the design feasibility of the UAV. The prototype proved to function as planned, capable of gliding, powered flight, and takeoff.


2021 ◽  
Author(s):  
Yukei Oyama

This undergraduate paper demonstrates the design, analysis, and manufacturing of a rocket deployable electric powered experimental unmanned aerial vehicle. The design process begins with defining the volume and dimensions of the allocated payload space for the UAV in the rocket. These dimensions are given by the aerostructures sub team in the Ryerson Rocketry Club. The dimensions given were used to determine the best configuration for the mission. The wing loading, power loading and endurance of the UAV are obtained from the constrained payload volume in the rocket and the avionics system of the of the UAV. The wing area, UAV weight and power requirements were calculated based on the previously determined values. The power requirement determines the motor size and propeller configuration. Aerodynamics, stability, and control were based the selected airfoil and obtained wing area. After completing the design, foam, additive manufacturing, and composite layups were used to create prototypes of the UAV. These prototypes were used to iterate the aircraft and address any immediate changes. The chosen design is a foldable flying wing, once deployed from the rocket has a wingspan of 70 inches, an aspect ratio of 13.35 and a surface area of 367 in2 . A prototype was created to prove the design feasibility of the UAV. The prototype proved to function as planned, capable of gliding, powered flight, and takeoff.


1995 ◽  
Vol 43 (6) ◽  
pp. 657 ◽  
Author(s):  
MP Rhodes

The wing morphology and flight performance of Phoniscus papuensis was examined to determine whether the wing morphology reflected published observations of flight behaviour and habitat preference. Wingspan and wing area were above the vespertilionid average for its mass. The wing loading and aspect ratio were below average. The wing loading is the lowest of any Australian vespertilionid. P. papuensis was able to successfully negotiate arrays of obstacles 22 cm apart 60% of the time. This ability, and the extremely broad, lightly loaded wings, afford the species unique flight characteristics which have been observed in the field and allow flight in complex, 'closed' habitats.


2010 ◽  
Vol 58 (5) ◽  
pp. 289 ◽  
Author(s):  
Darrell J. Kemp

Sexual competition promotes sexual selection and may influence the evolution of morphology, physiology and life history. In many flying insects, selection for efficient mate location is thought to have influenced male flight morphology in characteristic ways, with exponents of sit-and-wait tactics selected to possess high acceleration designs (i.e. high flight musculature and relatively small, elongate wings). However, many of these species also engage in elaborate and extended aerial disputes over territory ownership, and the need for contest ability may also select for a particular design. I attempted to tease apart the effects of these two influences by contrasting the flight morphology of two closely related Hypolimnas butterflies: H. bolina and H. alimena. While the males of both species rely predominantly on sit-and-wait tactics, only male H. bolina compete for territories via extended aerial manoeuvres. Males of this species possessed lower body mass per unit wing area (i.e. lower wing loading) and more elongate wings (i.e. higher aspect ratio), but did not differ from male H. alimena in relative flight musculature (thoracic mass). Males of both species varied from conspecific females in having higher relative flight musculature, lower wing loading and lower aspect ratio, which only partly supports expectations based solely upon sexual selection. These data suggest that selection for aerial contest ability may act weakly upon wing parameters, favouring a compromise between power/maneuverability and energetically efficient flight.


Author(s):  
Dorothy Taylor ◽  
Janice Morse ◽  
Andrew Merryweather

Elderly patient falls are expensive and may cause serious harm. Studies have identified the sit-to-stand-and-walk (STSW) task as the task where the greatest number of elderly patient falls occur. There is a great need to identify the particular movement and environmental conditions that lead to these elderly patient falls. This study begins to address this gap by evaluating the elderly patient during self-selected hospital bed egress. Using an observed fall risk episode (FRE) as a fall proxy, statistically significant parameters were identified which include bed height, pausing prior to initiating gait, level of fall risk, and Stand phase. Low bed height was identified as the least safe bed height. Patient-specific bed height (PSBH) using the patient’s lower leg length (LLL) is recommended. In addition, suggested guidelines are presented for clinical application in setting PSBH without measuring the patient’s LLL.


1970 ◽  
Vol 53 (2) ◽  
pp. 363-374 ◽  
Author(s):  
G. CHRISTIAN PARROTT

1. A black vulture (mass = 1.79 kg) gliding freely in a wind tunnel adjusted its wing span and wing area as its air speed and glide angle changed from 9.9 to 16.8 m/s and from 4.8° to 7.9°, respectively. 2. The minimum sinking speed was 1.09 m/s at an air speed of 11.3 m/s. 3. The maximum ratio of lift to drag forces was 11.6 at an air speed of 13.9 m/s. 4. Parasite drag coefficients for the vulture are similar to those for conventional airfoils and do not support the contention that black vultures have unusually low values of parasite drag.


2016 ◽  
Vol 64 (2) ◽  
pp. 701 ◽  
Author(s):  
Sebastián Montoya-Bustamante ◽  
Vladimir Rojas-Díaz ◽  
Alba Marina Torres-González

Coexistence of species from a trophic guild depends on the division and use of resources. In any ecosystem, fruits are resources that vary in time and space as well as in nutritional content. Therefore, the organisms that depend on them as a food source tend to show a certain degree of specialization. Understanding the factors that influence the dynamics of seed dispersal is important for the regeneration and conservation of tropical ecosystems. Our aim was to determine variation in consumption of <em>Piper tuberculatum </em>(pipilongo) by the fruit bat assemblages in the village of Robles (Jamundí, Valle del Cauca, Colombia). Pipilongo is a resource used not only by wildlife but also by people in the village of Robles. Bats were captured in mist nets between June and November 2014, their feces were collected, and the length of the forearm, wing area, leg length and weight were recorded. At the Universidad del Valle seed laboratory, fecal samples were washed, and their content determined. Of the 14 species captured, <em>Sturnira lilium, Carollia brevicauda, Carollia perspicillata</em> and <em>Artibeus lituratus</em> showed signs of having consumed <em>P. tuberculatum.</em> <em>Sturnira lilium</em> was the main consumer of <em>P. tuberculatum </em>fruits, with the greatest number of consumption events of fruit from this plant species, whereas the other bats showed more diversified consumption events. The greatest niche overlap was recorded between <em>C. brevicauda</em> and <em>C. perspicillata</em>, species that showed similar sizes (i.e., wing area and forearm length) followed by <em>S. lilium</em> and <em>C. perspicillata. </em>In contrast, <em>A. lituratus</em> showed the least niche overlap with the other three fruit bats captured. In conclusion, <em>Sturnira lilium</em> showed an interaction <em>Sturnira-Piper</em>, which is the result of low <em>Solanum</em> availability, and this bat species was the largest consumer of pipilongo in the region.


1958 ◽  
Vol 35 (2) ◽  
pp. 280-285
Author(s):  
B. G. NEWMAN

1. The soaring and gliding performance of the black vulture has been analysed and the following conclusions are drawn. 2. The wing span of the bird is altered in flight so that it may perform two tasks efficiently. First, that it may soar in rising currents of air for which a low sinking speed and thus a large wing span are required. Secondly, that it may penetrate into wind without undue loss of height for which a reduced wing area is desirable. Adjustment of the wing geometry towards the optimum soaring configuration is achieved by bending forward and opening the primary tip feathers. 3. Since the airflow readily separates from the flat primary feathers at high angle of attack, these feathers, which are emarginated, are parted to form slots. The alula also presumably assists in delaying the flow separation over the primaries. 4. It is unlikely that the opening of the primaries reduces the vortex drag.


2019 ◽  
Vol 15 (3) ◽  
pp. 20180857 ◽  
Author(s):  
Lucila I. Amador ◽  
Nancy B. Simmons ◽  
Norberto P. Giannini

Bats are the only mammals capable of powered flight. One of the oldest bats known from a complete skeleton is Onychonycteris finneyi from the Early Eocene (Green River Formation, Wyoming, 52.5 Ma). Estimated to weigh approximately 40 g, Onychonycteris exhibits the most primitive combination of characters thus far known for bats. Here, we reconstructed the aerofoil of the two known specimens, calculated basic aerodynamic variables and compared them with those of extant bats and gliding mammals. Onychonycteris appears in the edges of the morphospace for bats, underscoring the primitive conformation of its flight apparatus. Low aerodynamic efficiency is inferred for this extinct species as compared to any extant bat. When we estimated aerofoil variables in a model of Onychonycteris excluding the handwing, it closely approached the morphospace of extant gliding mammals. Addition of a handwing to the model lacking this structure results in a 2.3-fold increase in aspect ratio and a 28% decrease in wing loading, thus greatly enhancing aerodynamics. In the context of these models, the rapid evolution of the chiropteran handwing via genetically mediated developmental changes appears to have been a key transformation in the hypothesized transition from gliding to flapping in early bats.


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