| Literature DB >> 32242240 |
Wei Liang1,2, Zhimin Liu1, Minghu Liu3, Xuanping Qin1,2, Carol C Baskin4,5, Jerry M Baskin4, Zhiming Xin3, Zhigang Wang3, Zhi Su3, Quanlai Zhou1.
Abstract
Lift-off velocity may be the most useful surrogate to measure the secondary dispersal capacity of diaspores. However, the most important diaspore attribute determining diaspore lift-off velocity is unclear. Furthermore, it is not known whether terminal velocity used to characterize the primary dispersal capacity of diaspores can also be used to predict their secondary wind dispersal capacity. Here, we investigate how diaspore attributes are related to lift-off velocity. Thirty-six species with diaspores differing in mass, shape index, projected area, wing loading, and terminal velocity were used in a wind tunnel to determine the relationship between diaspore attributes and lift-off velocity. We found that diaspore attributes largely explained the variation in lift-off velocity, and wing loading, not terminal velocity, was the best parameter for predicting lift-off velocity of diaspores during secondary wind dispersal. The relative importance of diaspore attributes in determining lift-off velocity was modified by both upwind and downwind slope directions and type of diaspore appendage. These findings allow us to predict diaspore dispersal behaviors using readily available diaspore functional attributes, and they indicate that wing loading is the best proxy for estimating the capacity for secondary dispersal by wind.Entities:
Keywords: Appendage type; diaspore mass; diaspore shape index; downwind slope; terminal velocity; upwind slope; wind tunnel; wing loading
Mesh:
Year: 2020 PMID: 32242240 PMCID: PMC7475251 DOI: 10.1093/jxb/eraa170
Source DB: PubMed Journal: J Exp Bot ISSN: 0022-0957 Impact factor: 6.992
Diaspore attributes relevant to wind dispersal of the 36 studied species (mean ±SE)
| Species | Appendage type | Mass (mg) | Projected area (mm2) | Shape index | Wing loading (mg mm−2) | Terminal velocity (m s−1) |
|---|---|---|---|---|---|---|
|
| Wing | 4.770±0.603 | 38.527±2.683 | 0.148±0.005 | 0.124±0.012 | 1.544±0.184 |
|
| 6.776±1.383 | 36.839±4.368 | 0.063±0.022 | 0.186±0.040 | 1.685±0.353 | |
|
| 9.905±1.807 | 25.481±2.892 | 0.152±0.011 | 0.394±0.086 | 2.428±0.270 | |
|
| 16.935±0.613 | 44.744±1.626 | 0.119±0.013 | 0.379±0.020 | 2.728±0.473 | |
|
| 17.090±1.754 | 191.062±11.037 | 0.173±0.003 | 0.090±0.010 | 1.043±0.060 | |
|
| 21.225±2.766 | 50.520±8.331 | 0.129±0.008 | 0.428±0.075 | 2.740±0.223 | |
|
| 31.350±8.569 | 77.276±13.293 | 0.007±0.005 | 0.409±0.093 | 2.485±0.228 | |
|
| 35.799±5.255 | 197.827±20.144 | 0.160±0.002 | 0.181±0.015 | 0.780±0.066 | |
|
| 52.095±4.929 | 166.598±16.548 | 0.002±0.003 | 0.314±0.028 | 2.255±0.164 | |
|
| 90.685±18.334 | 603.932±83.549 | 0.142±0.016 | 0.152±0.031 | 1.646±0.213 | |
|
| 149.975±25.795 | 218.669±26.680 | 0.003±0.003 | 0.686±0.082 | 3.098±0.141 | |
|
| 163.470±43.580 | 558.871±102.138 | 0.013±0.007 | 0.291±0.045 | 1.959±0.244 | |
|
| 178.635±20.052 | 765.118±85.573 | 0.167±0.004 | 0.237±0.043 | 2.475±0.385 | |
|
| 231.460±26.136 | 491.381±33.327 | 0.136±0.002 | 0.471±0.058 | 1.103±0.082 | |
|
| Thorn | 1.065±0.496 | 5.125±0.446 | 0.067±0.023 | 0.211±0.105 | 1.844±0.416 |
|
| 6.775±1.664 | 11.156±1.702 | 0.004±0.003 | 0.607±0.120 | 2.225±0.441 | |
|
| 16.155±2.413 | 15.584±2.210 | 0.056±0.006 | 1.039±0.074 | 3.090±0.266 | |
|
| 26.345±13.790 | 24.244±5.742 | 0.016±0.008 | 1.167±0.740 | 2.714±0.239 | |
|
| 44.420±10.625 | 73.215±16.064 | 0.007±0.004 | 0.615±0.122 | 3.285±0.116 | |
|
| 74.660±21.572 | 45.319±3.998 | 0.027±0.004 | 1.677±0.576 | 3.729±0.213 | |
|
| Hair | 1.120±0.233 | 24.731±5.720 | 0.057±0.021 | 0.046±0.010 | 0.622±0.111 |
|
| 2.340±1.109 | 203.032±43.006 | 0.001±0.002 | 0.013±0.008 | 0.315±0.045 | |
|
| 4.660±1.146 | 50.910±14.036 | 0.027±0.010 | 0.097±0.033 | 1.305±0.380 | |
|
| 5.005±1.227 | 73.216±16.911 | 0.194±0.004 | 0.069±0.015 | 1.078±0.173 | |
|
| 6.865±1.841 | 35.125±7.469 | 0.007±0.005 | 0.205±0.075 | 0.749±0.112 | |
|
| 9.115±1.860 | 40.598±4.212 | 0.006±0.004 | 0.227±0.055 | 2.195±0.225 | |
|
| 11.625±4.031 | 34.085±5.061 | 0.041±0.024 | 0.351±0.136 | 2.493±0.194 | |
|
| None | 1.115±0.239 | 1.388±0.160 | 0.031±0.009 | 0.819±0.231 | 0.551±0.031 |
|
| 2.320±0.221 | 5.668±0.425 | 0.092±0.004 | 0.410±0.039 | 0.660±0.044 | |
|
| 2.393±0.345 | 4.303±0.367 | 0.088±0.020 | 0.558±0.084 | 1.171±0.094 | |
|
| 5.165±0.403 | 8.218±0.635 | 0.101±0.005 | 0.631±0.057 | 1.258±0.461 | |
|
| 5.125±0.693 | 4.705±0.492 | 0.046±0.006 | 1.103±0.200 | 1.792±0.190 | |
|
| 18.185±3.573 | 9.322±0.781 | 0.019±0.003 | 1.956±0.378 | 2.858±0.371 | |
|
| 22.405±10.257 | 14.758±1.586 | 0.062±0.011 | 1.537±0.726 | 3.010±0.390 | |
|
| 40.865±10.544 | 20.209±2.554 | 0.041±0.009 | 2.037±0.526 | 2.470±0.252 | |
|
| 66.600±7.452 | 34.095±3.187 | 0.010±0.006 | 1.961±0.234 | 3.457±0.262 |
For each type of appendage, species are listed in order of increased mass.
The disc-shaped diaspore is shaped like ‘–’, with its two wings nearly on the same horizontal plane; the four-winged diaspore is shaped like ‘+’, with the adjacent wings at angles of 90°
Fig. 1.Diagram illustrating measurement of the diaspore lift-off velocity by wind tunnel. (1) Starting point section, (2) power section, (3 and 4) diversion section, (5) rectifying section, (6) transition section, (7) draft gear, (8) road wheel, (9) electric landing gear, (10) experimental section, (11) experimental section of wind tunnel, (12) pitot tube, (13) rubber tube, (14) differential pressure transmitter, (15) diaspore, (16) wire net.
The wind tunnel is 2 m in height, 2 m in width, and 20m in length. The upwind slope is 6–8º with the power section of wind tunnel at the lower part of the slope (a). The downwind slope is 6–8º with the power section at the upper part of the slope (b). The pitot tube was located 10 m away from the power section. It was inserted through the roof via the pitot hole, and wind speed was measured 1 m above the underlying surface (c).
Lift-off velocity of the 36 studied species on the upwind and downwind slope (mean ±SE)
| Species | Appendage type | Lift-off velocity (m s−1) | Significant difference | |
|---|---|---|---|---|
| Upwind slope | Downwind slope | |||
|
| Wing | 5.278±0.440 | 4.050±0.281 | *** |
|
| 4.197±0.338 | 3.585±0.150 | ** | |
|
| 7.023±0.717 | 5.962±0.469 | * | |
|
| 6.914±0.343 | 5.964±0.352 | ** | |
|
| 5.087±0.612 | 3.891±0.191 | ** | |
|
| 6.222±0.660 | 5.211±0.227 | * | |
|
| 5.537±0.167 | 3.470±0.131 | *** | |
|
| 8.797±0.207 | 5.294±1.044 | *** | |
|
| 4.876±0.316 | 3.715±0.127 | *** | |
|
| 4.892±0.299 | 3.764±0.204 | *** | |
|
| 5.937±0.495 | 3.878±0.529 | *** | |
|
| 4.443±0.229 | 3.523±0.253 | *** | |
|
| 4.955±0.408 | 3.701±0.248 | *** | |
|
| 11.069±0.662 | 10.109±1.155 | NS | |
|
| Thorn | 5.332±0.174 | 4.268±0.368 | *** |
|
| 5.887±0.964 | 4.944±0.148 | NS | |
|
| 6.822±0.180 | 5.482±0.303 | *** | |
|
| 8.809±0.463 | 6.368±0.312 | *** | |
|
| 5.774±0.230 | 4.273±0.541 | *** | |
|
| 11.284±0.816 | 10.436±0.634 | NS | |
|
| Hair | 2.582±0.004 | 2.517±0.093 | NS |
|
| 2.108±0.002 | 2.306±0.130 | ** | |
|
| 3.125±0.344 | 2.610±0.214 | * | |
|
| 4.195±0.298 | 3.622±0.116 | ** | |
|
| 3.192±0.193 | 2.624±0.183 | ** | |
|
| 4.416±0.284 | 3.151±0.116 | *** | |
|
| 3.689±0.467 | 3.292±0.228 | NS | |
|
| None | 5.617±0.731 | 5.540±0.440 | NS |
|
| 7.104±0.525 | 6.447±0.214 | * | |
|
| 5.572±0.783 | 7.422±0.177 | NS | |
|
| 5.107±0.426 | 5.016±0.529 | NS | |
|
| 9.891±0.377 | 9.550±0.278 | NS | |
|
| 10.659±0.661 | 9.227±0.415 | ** | |
|
| 7.577±0.947 | 6.654±0.541 | NS | |
|
| 12.324±0.217 | 11.333±0.340 | *** | |
|
| 9.462±1.235 | 6.987±0.790 | ** |
For each type of appendage, species are listed in order of increased mass.
The disc-shaped diaspore is shaped like ‘–’, with its two wings nearly on the same horizontal plane; the four-winged diaspore is shaped like ‘+’, with the adjacent wings at angles of 90°. *0.011
Percentage of total variation of lift-off velocity on the upwind slope and downwind slope explained by wing loading, terminal velocity, diaspore mass, projected area, and shape index
| Diaspore attributes | Upwind slope | Downwind slope | ||||
|---|---|---|---|---|---|---|
| Explanation % |
|
| Explanation % |
|
| |
|
| 77.3 | 54.4 | 0.001** | 76.0 | 50.3 | 0.001** |
|
| 22.1 | 7.2 | 0.014* | 12.6 | 3.7 | 0.060 |
|
| 7.1 | 2.0 | 0.164 | 3.7 | 1.0 | 0.328 |
|
| 1.5 | 0.4 | 0.551 | 3.2 | 0.9 | 0.387 |
|
| <0.1 | <0.1 | 0.883 | <0.1 | <0.1 | 0.909 |
|
| 79.6 | – | – | 78.5 | – | – |
The total explanation of the diaspore attributes on variation of lift-off velocity was calculated by the canonical correlation analysis.
*0.011
Correlation matrix between diaspore attributes and lift-off velocity parameters
| Lift-off velocity | Diaspore mass | Projected area | Shape index | Wing loading | Terminal velocity | |||||
|---|---|---|---|---|---|---|---|---|---|---|
|
| Significance |
| Significance |
| Significance |
| Significance |
| Significance | |
|
| 0.237 | 0.164 | –0.110 | 0.523 | 0.026 | 0.879 |
| 0.000 |
| 0.011 |
|
| 0.170 | 0.320 | –0.159 | 0.354 | 0.021 | 0.905 |
| 0.000 | 0.314 | 0.062 |
|
| 0.262 | 0.123 | 0.140 | 0.414 | 0.007 | 0.966 | 0.208 | 0.224 |
| 0.013 |
|
| 0.298 | 0.300 | –0.004 | 0.989 | 0.344 | 0.228 | 0.348 | 0.222 | –0.316 | 0.270 |
|
| 0.781 | 0.067 | 0.232 | 0.658 | –0.144 | 0.786 |
| 0.004 | 0.670 | 0.146 |
|
| 0.695 | 0.083 | –0.519 | 0.233 | 0.407 | 0.365 | 0.553 | 0.198 | 0.734 | 0.060 |
|
| 0.566 | 0.112 | 0.473 | 0.198 | –0.571 | 0.108 |
| 0.012 | 0.638 | 0.064 |
|
| 0.337 | 0.238 | 0.028 | 0.924 | 0.363 | 0.202 | 0.339 | 0.235 | –0.250 | 0.389 |
|
| 0.792 | 0.060 | 0.205 | 0.697 | –0.084 | 0.874 |
| 0.012 | 0.660 | 0.154 |
|
| 0.601 | 0.153 | –0.368 | 0.417 | 0.682 | 0.091 | 0.458 | 0.302 | 0.644 | 0.118 |
|
| 0.313 | 0.412 | 0.213 | 0.582 | –0.408 | 0.275 | 0.614 | 0.079 | 0.423 | 0.257 |
|
|
| 0.043 | 0.052 | 0.796 | 0.205 | 0.305 |
| 0.000 |
| 0.023 |
|
|
| 0.048 | 0.034 | 0.868 | 0.195 | 0.331 |
| 0.000 |
| 0.040 |
|
|
| 0.023 | 0.233 | 0.308 |
| 0.029 |
| 0.009 | 0.210 | 0.362 |
|
|
| 0.023 | 0.218 | 0.343 |
| 0.028 |
| 0.021 | 0.136 | 0.557 |
Up, lift-off velocity of diaspore on the upwind slope; Down, lift-off velocity of diaspore on the downwind slope; Up–down, difference between lift-off velocity on the upwind and downwind slope; Appendage, diaspores with any appendages (wings, thorn, or hairs); Fly, diaspores with wings or hairs; Wing, Thorn, Hair; and None, diaspores with wings, thorns, hairs, and without any appendages, respectively. *0.011
Fig. 2.Relationship between lift-off velocities on upwind (a, c) and downwind (b, d) slopes, and wing loading and terminal velocity for diaspores with different types of appendage. Values shown were mean ±SE. Total, Thorn, None, Appendage, and Fly, diaspores of all 36 species, diaspores with thorns, diaspores without appendages, diaspores with any appendages (wings, thorns, or hairs), and diaspores with wings or hairs, respectively. Solid regression lines correspond to 36 species (squares), short-dashed lines to diaspores with thorns (triangles), long-dashed lines to diaspores without any appendages (circles), short-dotted lines to diaspores with appendages (rhombi), and dash–dot lines to diaspores with appendages (pentagrams).
Significant linear regression between lift-off velocity and wing loading of diaspores with different appendage types on upwind and downwind slopes
| Appendage type | Upwind slope | Downwind slope | ||||
|---|---|---|---|---|---|---|
| Regression equation |
|
| Regression equation |
|
| |
|
|
| 0.3081 | 0.009 |
| 0.2492 | 0.021 |
|
|
| 0.8963 | 0.004 |
| 0.8232 | 0.012 |
|
|
| 0.4980 | 0.000 |
| 0.4960 | 0.000 |
|
|
| 0.6153 | 0.000 |
| 0.5968 | 0.000 |
|
|
| 0.6171 | 0.012 | – | – | – |
Total, diaspores of all species; Appendage, diaspores with any appendages (wings, thorn, or hairs); Fly, diaspores with wings or hairs; Thorn, diaspores with thorns; None, diaspores without any appendages.
Significant linear regression between lift-off velocity and terminal velocity of diaspores with different appendage types on upwind and downwind slopes
| Appendage type | Upwind slope | Downwind slope | ||||
|---|---|---|---|---|---|---|
| Regression equation |
|
| Regression equation |
|
| |
|
|
| 0.1756 | 0.023 |
| 0.1576 | 0.040 |
|
|
| 0.1756 | 0.011 | – | – | – |
|
|
| 0.6171 | 0.012 | – | – | – |
Total, diaspores of all species; Appendage, diaspores with any appendages (wings, thorn, or hairs); None, diaspores without any appendages