Abstract
Several species of stalk-eyed flies exhibit exaggerated sexual dimorphism where females favor males with longer eyespans. Longer eyespan increases a fly’s moment of inertia, and may, therefore, impact flight behavior and fitness, specifically maneuverability and predator evasion. However, these putative costs may be ameliorated by co-selection for compensatory traits, as flies with longer eyespans tend to have larger thoraces and wings, which allows them to perform turns similar to flies with shorter eyespans. Furthermore, the capacity to compensate for a potentially costly ornament may not be fixed across the life-history of the adult stage, as stalk-eyed flies achieve sexual maturity at 3-4 weeks of age, accompanied by significant growth of reproductive tissues and organs. Thus, growth of the abdomen and body mass over time may impose constraints on flight performance that may affect whether an adult reaches the age of reproductive viability. The purpose of this study was to investigate the flight performance of stalk-eyed flies and its relationship to body morphology and development. The flight performance of 1-to-30 day old Teleopsis dalmanni (n=124) and Diasemopsis meigenii (n=83) were assessed by presenting normoxic, variable-density mixtures of heliox (O2, N2 and He) in 10% increments ranging from air to pure heliox; the least-dense gas allowing flight represented maximal performance. Flight kinematics were analyzed using high-speed (5930fps) videography. Immediately following flight assessment, flies were euthanized, photographed, dissected and weighed. In both species, total body mass, thorax and abdominal mass increased across age. Wing kinematics and maximal flight capacity were associated with thorax mass, and increased with age as flies became heavier. Although flies with longer eyespans were indeed heavier, they had larger wings and thoraces; however, maximal flight capacity and kinematics were generally independent of eyespan. Thus, bearing long eye-stalks did not impair flight performance, nor did the increase in mass attributable to reproductive maturation. Instead, variation in flight performance appears associated with the development of the flight motor, and improved ratio of thorax-to-total mass, across age.
1 Introduction
Communication between rivals or potential mates is often accomplished with extremely exaggerated ornaments and armaments in elaborate displays, and the evolution of such signals has received significant attention (; ). Nevertheless, despite decades of research aiming to explain how such traits evolve, one of the most elusive questions in animal behavior is how the use of ornaments during mate choice and rival assessment remains a reliable signal over evolutionary time. The predominant hypothesis posits that ornaments are costly to those that bear them (Zahavi, 1975), though this itself remains controversial (Számadó, 2010). Studies designed to test the prediction that ornaments should be costly to their bearer have often failed to measure significant performance costs (), particularly those using Morphology → Performance → Fitness framework. Indeed, despite the intuitive notion that exaggerated ornaments should impact locomotor performance and behaviors by placing an evolutionary constraint on the evolution of ornaments, extreme exaggeration of ornaments has often evolved with little or no measurable decrease in performance (; ).
proposed modifications to framework to account for female choice of ornaments, or use of ornaments to assess rivals, where direct selection on morphology interacts with the detrimental effects of the ornament to indirectly drive the evolution of performance (Figure 1). This modification recognizes that natural selection may limit elaboration and exaggeration of ornaments (; )and considers there may also be selection on the integrated whole organism, including elements that reduce the negative effects of sexually selected traits such as ornaments. Specifically, there may be correlated selection for compensatory traits (; ; ; ; Swallow et al., 2009), which may occur at multiple stages of development and life history (Stearns, 1992; ; ; ).
Figure 1
Stalk-eyed flies (family Diopsidae) are a tractable model-system to explore the interaction between a detrimental, sexually-selected ornament and morphological traits that offset performance costs. These dipterans possess peculiar head morphology (Figure 2A), with eyes located laterally on long stalks (
Figure 2

Description of methods. (A) The flight performance of male Teleopsis dalmanni (right; n=123) and Diasemopsis meigenii (left; n=84) were assessed using (B) hypodense, normoxic mixtures of oxygen, nitrogen and helium in an 8-liter cylindrical flight chamber. A high-speed video camera (5930 fps) oriented above the chamber recorded hovering flight. (C) The hovering sequences were digitized, and wing stroke amplitude was calculated from the horizontal angular displacement of the dorsal and ventral wing stroke reversals.
Although larger eyespans increase mating success (
Stalk-eyed flies do not reach sexual maturity until about 3-4 weeks of age, post-eclosion. Many studies investigating competition or mating behaviors of stalk-eyed flies have focused on sexually-mature adults, as these behaviors would likely occur at lesser frequency in sexually-immature individuals (
The purpose of this study is to characterize the allometry of morphology and flight performance of male stalk-eyed flies, Teleopsis dalmanni and Diasemopsis meigenii, across age. Both are dimorphic species where female sexual preference has driven the exaggeration of male eyespan, and where thorax and wing morphology appears to have co-evolved with eyespan, putatively as a compensatory mechanism (
2 Materials and methods
Populations of stalk-eyed fly species Teleopsis dalmanni and Diasemopsis meigenii were maintained in an environmentally-controlled room at 24C, 80% relative humidity and a 12h/12h light-dark cycle. Adult flies were collected within one day post-eclosion and housed in 3L chambers, separated by age and species. Flies were fed a diet of pureed corn and instant Drosophila food ad libitum, and food cups were replaced every 4 days. Male flies that possessed intact wings and were free of morphological defect (e.g. malformed abdomens, missing legs, etc.) were selected for assessment of flight performance and allometry.
Flight performance was assessed individually (i.e. one fly in the chamber at a time) using variable density, normoxic gas mixtures which consisted of oxygen and nitrogen and/or helium (
Table 1
| Heliox % | ρ kg m-3 | Gas Fraction | ||
|---|---|---|---|---|
| O2 % | N2 % | He % | ||
| 0 (air) | 1.21 | 21.0 | 79.0 | 0 |
| 10 | 1.13 | 21.0 | 71.1 | 7.9 |
| 20 | 1.05 | 21.0 | 63.2 | 15.8 |
| 30 | 0.97 | 21.0 | 55.3 | 23.7 |
| 40 | 0.89 | 21.0 | 47.4 | 31.6 |
| 50 | 0.81 | 21.0 | 39.5 | 39.5 |
| 60 | 0.73 | 21.0 | 31.6 | 47.4 |
| 70 | 0.65 | 21.0 | 23.7 | 55.3 |
| 80 | 0.57 | 21.0 | 15.8 | 63.2 |
| 90 | 0.49 | 21.0 | 7.9 | 71.1 |
| 100 | 0.41 | 21.0 | 0 | 79.0 |
Variable-density gas mixtures presented to stalk-eyed flies.
Increasing percentage of heliox results in decreasing atmospheric density, which requires greater aerodynamic power to maintain hovering flight. Maximal flight capacity was determined to be the least-dense gas (LDG) allowing for flight.
The gasses were mixed using calibrated, solenoid-actuated valves (Tylan: FC-2910), which were plumbed into an 8L cylindrical acrylic chamber with an inlet port on the side for gas perfusion (Figure 2B). Gas mixtures and flow rates were metered by an electronic flow controller (Sable Systems MFC-4; Las Vegas, NV, USA). When changing the gas mixture, the flight chamber was flushed with the new gas mixture at a flow rate of 20L min-1 for 2 minutes to ensure complete washout. When assessing flight performance and filming hovering flight, total gas flow rate was maintained at 2L min-1. In any given gas mixture, flies were flown until sustained hovering flight was observed and recorded, or hovering flight was attempted but failed. Failure was typically distinguished by flies attempting to initiate flight from the floor of the chamber and being unable to reach at least the middle of the height of the chamber, thus excluding jumping and aerodynamic ‘ground effect’ from contributing to a potentially successful flight. Flies that landed on the floor or sides of the chamber were persuaded to fly by using a small magnetic stir-bar to chase and agitate them. Flies were excluded from the study if 1) they were unable to fly in air, or 2) they initially exhibited flight in air, but could not replicate flight in air after failing to fly in any of the hypodense gas mixtures. In this latter case, it was assumed that some other uncontrolled factor (e.g. motivation, injury, etc.) may have influenced the trial.
Hovering flight kinematics were determined from the wing motions in the horizontal plane, recorded by a high-speed (5930 fps) digital video camera (RedLake IDT MotionPro N3-S4). The camera was oriented above the flight chamber and focused such that the depth of field was in focus in the middle 1/3 of the chamber. Ascending, descending, maneuvers, and lateral flights (e.g. initiated at the side of the chamber, and flown directly across the chamber) were ignored. The digital video sequences were analyzed using DLTdv8 (
Following assessment of flight performance, flies were euthanized, weighed, dissected and photographed. Total body mass was obtained from the intact fly. The legs and wings were then removed, and the fly and wings were placed in the prone position on a slide-micrometer and photographed. The head, thorax, and abdomen were then separated and weighed. Photographs were analyzed using custom software (MatLab, The Mathworks) to determine eyespan (the distance from the lateral edges of the right and left eyes), thorax width, and the following wing morphometrics: wing-length, mean chord length, wing area, aspect ratio, and non-dimensional 2nd and 3rd moments of wing area (Vance and Roberts, 2014).
Multivariate analysis of covariance (MANCOVA, α=0.05) was used to evaluate the effect of species, eyespan and age (independent variables) on morphology and flight performance (dependent variables). Analysis of covariance (ANCOVA) was used to determine the effect of species and thorax mass, and the effect of species and wingtip velocity, on flight performance. Our post hoc analyses consisted of evaluating specific relationships using linear regression.
3 Results
3.1 Body and wing morphology
There was a significant effect of species, eyespan and age on body and wing morphology, and on body and segment masses (MANCOVA, Hotelling trace: P<0.001; Table 2). Although T. dalmanni had slightly longer (3%) eyespan, D. meigenii were generally larger and more massive: D. meigenii had 14% wider thoraces, 10% longer wings, 25% greater mean wing chord length, and 37% greater wing area than T. dalmanni. However, for distribution of wing area, T. dalmanni had 13% greater aspect ratio than D. meigenii; Though statistically significant, the differences in the non-dimensional 2nd and 3rd moments in wing area were small (<3%). D. meigenii had 44% heavier body mass than T. dalmanni, which consisted of 73% heavier heads, 54% heavier thoraces, 52% heavier abdomens, and 8% greater thorax mass-to-body mass ratio.
Table 2
| Parameter average (mean±s.d.) | Species | Eyespan | Age | |||||
|---|---|---|---|---|---|---|---|---|
| T. dalmanni | D. meigenii | F1,203 | P | F1,203 | P | F1,203 | P | |
| Morphology1 | ||||||||
| Eyespan (mm) | 7.98±0.37 | 7.81±0.26 | 13.9 | <0.001 | – | – | 1.10 | 0.292 |
| Thorax Width (mm) | 1.67±0.10 | 1.90±0.08 | 428.5 | <0.001 | 76.8 | <0.001 | 0.72 | 0.399 |
| R (mm) | 4.72±0.20 | 5.19±0.19 | 464.8 | <0.001 | 66.5 | <0.001 | 19.8 | <0.001 |
| Chord (mm) | 0.89±0.04 | 1.11±0.05 | 1740.7 | <0.001 | 80.0 | <0.001 | 19.1 | <0.001 |
| S (mm2) | 4.19±0.23 | 5.75±0.26 | 5575.0 | <0.001 | 374.5 | <0.001 | 0.03 | 0.852 |
| AR | 10.6±0.7 | 9.4±0.6 | 136.0 | <0.001 | 0.46 | 0.501 | 25.7 | <0.001 |
| r̂2(S) | 0.625±0.009 | 0.611±0.009 | 96.0 | <0.001 | 0.50 | 0.480 | 23.8 | <0.001 |
| r̂3(S) | 0.659±0.007 | 0.647±0.007 | 95.5 | <0.001 | 0.47 | 0.496 | 24.6 | <0.001 |
| Mass2 | ||||||||
| Mb (mg) | 6.19±1.13 | 8.91±1.52 | 986.0 | <0.001 | 130.1 | <0.001 | 304.9 | <0.001 |
| Mh (mg) | 0.62±0.09 | 1.07±0.13 | 2008.1 | <0.001 | 111.0 | <0.001 | 111.2 | <0.001 |
| Mt (mg) | 2.25±0.53 | 3.47±0.62 | 1244.8 | <0.001 | 134.3 | <0.001 | 422.1 | <0.001 |
| Ma (mg) | 1.81±0.53 | 2.75±0.72 | 384.2 | <0.001 | 38.4 | <0.001 | 177.5 | <0.001 |
| Mt: Mb | 0.36±0.03 | 0.39±0.02 | 118.8 | <0.001 | 2.6 | 0.105 | 86.2 | <0.001 |
Multivariate analysis of covariance (MANCOVA) for the effects of species, eyespan and age on body and wing morphology, and on body and segment mass.
1MANCOVA, Hotelling trace (body and wing morphology, except eyespan): Species, T2 = 6250.0, P<0.001; Eyespan, T2 = 523.6, P<0.001; Age, T2 = 41.5, P<0.001.
2MANCOVA, Hotelling trace (body and segment mass): Species, T2 = 2239.9, P<0.001; Eyespan, T2 = 243.4, P<0.001; Age, T2 = 456.1, P<0.001.
R, wing length; S, wing area; r̂2(S), non-dimensional 2nd moment of wing area; r̂3(S), non-dimensional 3rd moment of wing area; Mb, body mass; Mh, head mass; Mt, thorax mass; Ma, abdominal mass; Mt : Mb, thorax mass to body mass ratio.
Both species exhibited positive allometric trends in body morphology with respect to eyespan. Flies with longer eyespan had heavier heads (linear regression: T. dalmanni, R2 = 0.28, P<0.001; D. meigenii, R2 = 0.27, P<0.001), and tended to have heavier thoraces (T. dalmanni, R2 = 0.12, P<0.001; D. meigenii, R2 = 0.20, P<0.001) and abdomens (T. dalmanni, R2 = 0.07, P<0.001; D. meigenii, R2 = 0.07, P<0.012). Thus, flies with longer eyespans were generally heavier in overall body mass (linear regression: T. dalmanni, P<0.001, R2 = 0.28; D. meigenii, P<0.001, R2 = 0.19). Flies with longer eyespans had wider thoraces, longer wings and greater wing area (Figure S1). However, the distribution of wing area (e.g. aspect ratio, and non-dimensional 2nd and 3rd moments of wing area) were not associated with variation in eyespan (Table 3).
Table 3
| Parameter average (mean±s.d.) | Species | Eyespan | Age | |||||
|---|---|---|---|---|---|---|---|---|
| T. dalmanni | D. meigenii | F1,203 | P | F1,203 | P | F1,203 | P | |
| LDG (% Heliox) | 44.2±18.3 | 70.5±2.4 | 145.2 | <0.001 | 4.10 | 0.045 | 58.7 | <0.001 |
| nnorm (hz) | 157.2±17.2 | 153.6±13.7 | 27.3 | <0.001 | 0.34 | 0.559 | 630.4 | <0.001 |
| nmax (hz) | 160.2±18.2 | 162.1±17.1 | 83.3 | <0.001 | 0.016 | 0.901 | 582.5 | <0.001 |
| Φnorm (deg) | 151.0±8.0 | 157.6±8.7 | 21.1 | <0.001 | 0.38 | 0.540 | 5.6 | 0.019 |
| Φmax (deg) | 169.0±5.8 | 171.0±4.1 | 25.5 | <0.001 | 0.55 | 0.460 | 57.4 | <0.001 |
| Ut, norm (m sec-1) | 3.91±0.47 | 4.38±0.49 | 266.6 | <0.001 | 21.8 | <0.001 | 275.6 | <0.001 |
| Ut, max (m sec-1) | 4.47±0.65 | 5.03±0.65 | 332.1 | <0.001 | 12.9 | <0.001 | 499.1 | <0.001 |
Multivariate analysis of covariance (MANCOVA) for the effects of species, eyespan and age on flight performance.
MANCOVA, Hotelling trace: Species, T2 = 730.1, P<0.001; Eyespan, T2 = 88.1, P<0.001; Age, T2 = 890.8, P<0.001.
LDG, least-dense gas (maximal flight capacity); nnorm, wingbeat frequency in air; nmax, wingbeat frequency in LDG; Φnorm, wing stroke amplitude in air; Φmax, wing stroke amplitude in MGD; Ut, norm, wing velocity in air; Ut, max, wing velocity in LDG.
Both species exhibited positive allometry in body morphology with respect to age (Table 3). Body mass, and head, thorax and abdomen mass, increased with age (Figures 3A-D). The ratio of thorax mass-to-body mass increased across age in T. dalmanii and was generally maintained across age in D. meigenii (Figure 3E). Although there was a significant effect for age on wing length, mean chord length, and wing area distribution (Table 2), post hoc analyses revealed weak or non-significant linear regressions for these variables. Likewise, there was no effect of age on wing area (Table 2).
Figure 3

Body and segment masses for T. dalmanni (filled circles) and D. meigenii (open circles) increased with age (linear regression, p<0.001 for all comparisons). (A) Total body mass: T. dalmanni (solid line), Mb = 4.88 + 0.09age, R2 = 0.46; D. meigenii (dashed line), Mb = 7.01 + 0.20age, R2 = 0.59. (B) Head mass T. dalmanni (solid line), Mh = 0.56+.004age, R2 = 0.2; D. meigenii (dashed line), Mh = 0.94 + 0.013age, R2 = 0.40. (C) Thorax mass T. dalmanni (solid line), Mt = 1.58 + 0.04age, R2 = 0.56; D. meigenii (dashed line), Mt = 2.69 + 0.08age, R2 = 0.61. (D) Abdominal mass: T. dalmanni (solid line), Ma = 1.23 + 0.04age, R2 = 0.41; D. meigenii (dashed line), Ma = 1.89 + 0.09age, R2 = 0.55. (E) Thorax mass to body mass ratio: T. dalmanni (solid line), Mt: Mb = 0.33 + 0.002age, R2 = 0.37; D. meigenii (dashed line), Mt: Mb = 0.38 + 0.0007age, R2 = 0.05.
3.2 Flight performance and kinematics
There was a significant effect of species, eyespan and age on flight performance and kinematics (MANCOVA, Hotelling trace: P<0.001; Table 3). Wing kinematics during hovering in air were generally similar: T. dalmanni exhibited 2% greater wingbeat frequency and D. meigenii had 4% larger stroke amplitude. D. meigenii had 12% greater wing velocity than T. dalmanni, largely attributable to their longer wings. At maximal capacity, D. meigenii were able to fly in heliox mixtures that were 25% less-dense than T. dalmanni. This was facilitated by a relatively small increase in wingbeat frequency (<2% for T. dalmanni, 5% for D. meigenii), and a modest 12% and 8% increase in stroke amplitude for T. dalmanni and D. meigenii, respectively. This increase in kinematic output resulted in a 14-15% increase in wing velocity for both species in order to fly in the least dense gas (LDG).
There was no effect of eyespan on wingbeat frequency or stroke amplitude during normal or maximal hovering (Table 3). There was a significant, yet weak relationship between eyespan and wing velocity during normal and maximal hovering (Table 3), however linear regression revealed no significant trends between or across species (R2<0.02 for all comparisons). Likewise, there was a weak relationship between eyespan and maximal flight capacity, however linear regression revealed no significant trends between or across species (R2≤ 0.01 for all comparisons).
Maximal flight capacity increased with age in both species (linear regression: T. dalmanni, R2 = 0.20, P<0.001; D. meigenii, R2 = 0.32, P<0.001), and was positively associated with variation in body mass (linear regression: all flies, R2 = 0.42, P<0.001), thorax mass (linear regression: all flies, R2 = 0.49, P<0.001) and thorax mass-to-body mass ratio (T. dalmanni, R2 = 0.35, P<0.001; D. meigenii, R2 = 0.18, P<0.001). As flies aged, wingbeat frequency (T. dalmanni, R2 = 0.80, P<0.001; D. meigenii, R2 = 0.68, P<0.001), and wing velocity (T. dalmanni, R2 = 0.73, P<0.001; D. meigenii, R2 = 0.70, P<0.001) increased during both normal and maximal flight (Table 3). Maximal flight capacity was positively associated with thorax mass and wingtip velocity (Figure 4; ANCOVA: P<0.001 for both comparisons; linear regression: R2 = 0.49 and 0.53, respectively, P<0.001). Thus, as thorax mass increased, wingbeat frequency increased (linear regression: T. dalmanni, R2 = 0.63, P<0.001; D. meigenii, R2 = 0.63, P<0.001) and wing velocity increased (Figure 4), which facilitated the improvement in maximal flight capacity.
Figure 4

Effects of Morphology on Flight Performance in T. dalmanni (filled circles) and D. meigenii (open circles). Maximal flight capacity, LDG, is defined as the least dense gas allowing for flight, where 0% Heliox is air (21% O2, 79% N2, 0% He; density: 1.21 kg m-3) and 100% is pure Heliox (21% O2, 0% N2, 79% He; density: 0.41 kg m-3). (A) Wingtip velocity increased across thorax mass in both species (P<0.001): linear regression: T. dalmanni (solid line), Ut = 2.13 + 1.04Mt, R2 = 0.72; D. meigenii (dashed line), Ut = 2.11 + 0.84Mt, R2 = 0.65. (B) Maximal flight capacity (LDG, in percent-heliox) increased across wingtip velocity for both species (P<0.001); linear regression: LDG = -6.5 + 2.55Ut, R2 = 0.53. (C) Maximal flight capacity (LDG, in percent-heliox) increased across thorax mass for both species (P<0.001); linear regression: LDG = -0.28 + 2.1Mt, R2 = 0.49.
4 Discussion
Stalk-eyed flies reach sexually maturity 3- to 4-weeks post-eclosion (
The development of the thorax facilitated an improvement in wingbeat frequency with age. The mass of the thorax cuticle and wings are presumably fixed post-eclosion, and the mechanical properties of resonating and reciprocating passive structures are likewise presumed constant post-sclerotization. Age-dependent improvements in the performance of the flight motor in adults have been observed in several orders of insects. Physiological changes often occur soon after eclosion and/or the onset of flight-dependent behaviors, and may include alternative splicing of troponin variants which affect muscle calcium sensitivity (
Nonetheless, the two-fold increase in thorax mass we observed across age in adult stalk-eyed flies was unexpected. Given the lekking behavior and general localization of lek sites where T. dalmanni and D. meigenii aggregate, we suspect lipid stores to support flight endurance were not the main constituents of this increased thorax mass; rather, we posit this thoracic development results from investment in muscle mass, and subsequent increased muscle stiffness and power to drive the indirect actuation of the wings (Figure 4A). As flies were able to generate greater wing velocity as their thorax mass increased, they were able to produce greater aerodynamic power, resulting in increased maximal flight capacity (Figures 4B, C). Thus, as flies became heavier with age, in part due to the growth of reproductive tissues in the abdomen, the concurrent development of the thorax compensated for this growth and is associated with increased maximal flight capacity across age (Table 3).
Studies of sexually-mature, adult stalk-eyed flies suggest thorax and wing size have co-evolved with eyespan as a mechanism to compensate for the inertial and aerodynamic costs associated with bearing larger ornaments and having a larger body (
Our findings generally support prior conclusions, as individual T. dalmanni and D. meigenii with larger eyespan had wider thoraces and larger wings, and were generally heavier. Thus, within this sample, one might predict compensation by comparing relative ornament size to relative trait size (
As adult T. dalmanni and D. meigenii males aged, they became stronger fliers. This age-related variation in flight performance critically depends on the development of the thorax, specifically the flight muscle. In this study, the pace of thorax development compensated for the pace of sexual development (i.e. abdominal mass), such that the ratio of thorax mass to body mass was maintained (D. meigenii) and/or increased (T. dalmanni) across age (Figure 3E). If the development of reproductive tissues were prioritized over muscle development, flies may not maintain the ratio of thorax mass to total body mass necessary to improve -or perhaps even conserve- flight capacity as they approach sexual maturity. For example, if 25- to 30-day old T. dalmanni in this study did not exhibit thorax development, but instead maintained thorax mass similar to <5-day old flies, their thorax-to-body mass ratio would be reduced by 31%, as would their ability to generate wing velocity to compensate for their increased body mass across age. Time to sexual maturity and mating frequency critically depends on the growth of the accessory glands (
Finally, consider that the flies in this study were fed ad libitum and were not crowded in their enclosures: our findings may reflect an ideal or optimal scenario for the development of flight muscle. If, instead, food availability was scarce, nutritionally deficient, or subject to strong competition, how might the development of the thorax compare to the development of the abdomen? Deriving fitness from proxies of survival and fecundity gleaned from sexually-mature flies may represent a best-case scenario for the relationships between compensatory traits and ornaments, as such experiments select flies that have made it through a potentially-costly period of development. However, it cannot necessarily extrapolate to prior developmental periods, where age-related fecundity depends on the growth of reproductive tissues (
Assessing the costs of bearing ornaments has been elusive where morphological traits and behaviors may compensate for impairments (
Statements
Data availability statement
The raw data supporting the conclusions of this article will be made available by the authors, without undue reservation.
Author contributions
JV and JS contributed to the conception and design of the study. JV and KP performed the experiment and analyzed the data. JV, CA, and JS wrote the manuscript. All authors contributed to the article and approved the submitted version.
Funding
This research was funded by a National Science Foundation grant (NSF IOS 1656478) to JV, and a National Science Foundation grant (NSF IOS 1656465) to JS.
Acknowledgments
The authors acknowledge that neither ChatGPT, nor any LLM, was used in the preparation or editing of this manuscript.
Conflict of interest
The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be constructed as a potential conflict of interest.
The author JS declared that they were an editorial board member of Frontiers, at the time of submission. This had no impact on the peer review process and the final decision.
Publisher’s note
All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.
Supplementary material
The Supplementary Material for this article can be found online at: https://www.frontiersin.org/articles/10.3389/fetho.2023.1242198/full#supplementary-material
Supplementary Figure 1Allometry of stalk-eyed flies, T. dalmanni (filled circles) and D. meigenii (open circles). (A)Thorax width in both species increased with eyespan (P<0.001). Linear regression: T. dalmanni (solid line), thorax width = 0.45 + 0.15eye, R2 = 0.30; D. meigenii (dashed line), thorax width = 0.82 + 0.14eye, R2 = 0.20. (B)Wing length in both species increased with eyespan (P<0.001). Linear regression: T. dalmanni (solid line), wing length = 2.53 + 0.27eyespan, R2 = 0.25; D. meigenii (dashed line), wing length = 2.98 + 0.28eye, R2 = 0.16. (C)Wing area in both species increased with eyespan (P<0.001). Linear regression: T. dalmanni (solid line), wing area = 0.04 + 0.52eyespan, R2 = 0.69; D. meigenii (dashed line), S = -0.47 + 0.80eye, R2 = 0.66.
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Summary
Keywords
sexual selection, ornaments, compensation, flight performance, stalk-eyed flies
Citation
Vance JT, Pehl K, Acakpo CJ and Swallow JG (2023) Compensation for a costly ornament depends on the development of flight performance in stalk-eyed flies. Front. Ethol. 2:1242198. doi: 10.3389/fetho.2023.1242198
Received
18 June 2023
Accepted
18 September 2023
Published
03 October 2023
Volume
2 - 2023
Edited by
Gordon M. Burghardt, The University of Tennessee, Knoxville, United States
Reviewed by
Lee Drickamer, Northern Arizona University, United States; Richard Baker, American Museum of Natural History, United States
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© 2023 Vance, Pehl, Acakpo and Swallow.
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*Correspondence: Jason T. Vance, vancejt@cofc.edu
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