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Number Words 1-20 Worksheets - Planes Balloons
17. Comparison of simulated and measured radiation patterns of the proposed antenna (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 18. 3D radiation patterns of the wearable textile antenna: (a) 1.8 GHz, (b) 2.45 GHz, (c) 5.8 GHz. Figure 18. 3D radiation patterns of the wearable textile antenna: (a) 1.8 GHz, (b) 2.45 GHz, (c) 5.8 GHz. Figure 19. Comparison of measured radiation patterns in different bending scenarios (at 25 mm, 35 mm, and 45 mm) (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 19. Comparison of measured radiation patterns in different bending scenarios (at 25 mm, 35 mm, and 45 mm) (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 20. Simulated vs. measured efficiency of the proposed wearable antenna. Figure 20. Simulated vs. measured efficiency of the proposed wearable antenna. Figure 21. Simulated average SAR distribution on the cuboid phantom: at (a) 1.8 GHz (b) 2.45 GHz (c) 5.8 GHz. Figure 21. Simulated average SAR distribution on the cuboid phantom: at (a) 1.8 GHz (b) 2.45 GHz (c) 5.8 GHz. Figure 22. Link margin between Tx (proposed ant.) and Rx (monopole ant.) antennas at 1.8/2.45/5.8 GHz frequency bands. Figure 22. Link margin between Tx (proposed ant.) and Rx (monopole ant.) antennas at 1.8/2.45/5.8 GHz frequency bands. Table 1. Proposed antenna and previously reported textile antennas. Table 1. Proposed antenna and previously reported textile antennas. Ref. (Year)[19](2020)[20](2021)[21](2022)[22](2022)[23](2023)This WorkArea(mm2)65 × 6060 × 6060 × 6055 × 4084 × 6960 × 60Area(λ02)0.18 × 0.17(0.03)0.49 × 0.49(0.24)0.64 × 0.64(0.41)1.46 × 1.06(1.55)0.55 × 0.67(0.37)0.36 × 0.36(0.13)Frequency (GHz)0.868/2.452.45/3.452.4/3.32/3.93/5.882.4/51.8/2.45/5.8B.W. (%)NG/3.54.9/6.73.7/5.7/5.85/9.813.15/7617.2/39.1/19.6Peak gain (dBi)NG/−1.46.7/8.9−0.81/−2.81/−1.16/2.85.27.23.7/5.3/9.6SAR (W/Kg)1 gm/10 gmNG0.1/0.04(at 0.5 W)0.11/0.33(at 1 W)0.7/---(at 1 W)NG0.0796/0.07590.0575/0.05520.0226/0.0204(at 1 W) Table 2. Antenna’s design parameters (in mm). Table 2. Antenna’s design parameters (in mm). SymbolValueSymbolValueSymbolValueSymbolValueL60L718WF3.6X118.5LP50L813W1–W66.0X234.5LF15L918W705X321.0L125L1012W811X417.0L209L113.0W903X57.5L303L1208W1011Y14.0L407L1338W1103Y2–Y45.0L503W60W1206 L63.5WP40W1331 Table 3. Boresight peak gain values (dBi). Table 3. Boresight peak gain values (dBi). Frequency(GHz)Simulation(Chest Phantom)Measured(on Human Chest)1.83.72.82.455.34.65.89.68.2 Table 4. Boresight peak gain values (dBi) at different bending radii: 45 mm, 35 mm, and 25 mm. Table 4. Boresight peak gain values (dBi) at different bending radii: 45 mm, 35 mm, and 25 mm. Frequency (GHz)At 45 mmAt 35 mmAt 25 mm1.82.12.00.2 2.454.54.63.25.88.28.17.8 Table 5. Maximum SAR of the proposed antenna (at 1 W input power). Table 5. Maximum SAR of the proposed antenna (at 1 W input power). Frequency(GHz)Maximum SAR (on Phantom)1 gm10 gm1.80.07960.07592.450.05750.05525.80.02260.0204 Table 6. Link budget parameters. Table 6. Link budget parameters. Transmitter Frequency (GHz)1.8/2.45/5.8GtAntenna gain (dBi)3.7/5.3/9.6PtTransmitted power (dBm)16 EIRP (dBm)19.7/21.3/25.6ReceiverGrReceiver antenna gain (dBi)(external antenna)2.15ToAmbient temperature (K)293 Boltzmann constant1.38 × 10−23NoNoise power density (dB/Hz)−203.9Signal qualityBrBit rate (Mbps)0.250, 1, 10 Eb/NoIdeal PSK (dB)9.6GcCoding gain (dB)0GdFixing deterioration (dB)2.5 Disclaimer/Publisher’s Note: The statements, opinions and data contained in Download a sound effect to use in your next project. Royalty-free sound effects. Big Plane Sound Effect TanwerAman. 0:20. Plane Aircraft Planes. 24. Prop Plane freesound_community. 1:54. Engine Flying Prop. 25. Plane Sound From Distance HQ TanwerAman. 0:20. Plane Aircraft Planes. 6. Plane takeoff freesound_community. 1:21. 137, 104301. [Google Scholar] [CrossRef]Zhang, K.Y.; Wang, Y.; Ai, Y.B. Analytical solution to interaction between pipelines and soils under arbitrary loads. Chin. J. Geotech. Eng. 2010, 32, 1189–1193. (In Chinese) [Google Scholar]Zhao, M.; Xu, L.; Huang, J.; Du, X.; Li, H. Analytical solutions of the tunnels under the fault creeping by elastic foundation beam model with considering tangential interaction. Soil Dyn. Earthq. Eng. 2023, 172, 108047. [Google Scholar] [CrossRef] Figure 1. Displacement of the free field. Figure 1. Displacement of the free field. Figure 2. Euler beam on the Winkler foundation. Figure 2. Euler beam on the Winkler foundation. Figure 3. A double cosine load applied on the plane xoy. Figure 3. A double cosine load applied on the plane xoy. Figure 4. A simple cosine load acting on a foundation. Figure 4. A simple cosine load acting on a foundation. Figure 5. Displacement coordination of the beam and ground. Figure 5. Displacement coordination of the beam and ground. Figure 6. Three-dimensional solid finite element model. Figure 6. Three-dimensional solid finite element model. Figure 7. Beam–spring numerical model. Figure 7. Beam–spring numerical model. Figure 8. Beam displacement along the axis obtained via different methods [20]. Figure 8. Beam displacement along the axis obtained via different methods [20]. Figure 9. Beam internal forces along the axis obtained using different methods (a) bending moment; (b) shear force [20]. Figure 9. Beam internal forces along the axis obtained using different methods (a) bending moment; (b) shear force [20]. Figure 10. The errors of the tunnel’s peak internal forces along the axis using different elastic moduli: (a) bending moment; (b) shear force [20]. Figure 10. The errors of the tunnel’s peak internal forces along the axis using different elastic moduli: (a) bending moment; (b) shear force [20]. Table 1. Fitting data from the twoComments
17. Comparison of simulated and measured radiation patterns of the proposed antenna (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 18. 3D radiation patterns of the wearable textile antenna: (a) 1.8 GHz, (b) 2.45 GHz, (c) 5.8 GHz. Figure 18. 3D radiation patterns of the wearable textile antenna: (a) 1.8 GHz, (b) 2.45 GHz, (c) 5.8 GHz. Figure 19. Comparison of measured radiation patterns in different bending scenarios (at 25 mm, 35 mm, and 45 mm) (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 19. Comparison of measured radiation patterns in different bending scenarios (at 25 mm, 35 mm, and 45 mm) (a) H-plane at 1.8 GHz (b) E-plane at 1.8 GHz (c) H-plane at 2.45 GHz (d) E-plane at 2.45 GHz (e) H-plane at 5.8 GHz (f) E-plane at 5.8 GHz. Figure 20. Simulated vs. measured efficiency of the proposed wearable antenna. Figure 20. Simulated vs. measured efficiency of the proposed wearable antenna. Figure 21. Simulated average SAR distribution on the cuboid phantom: at (a) 1.8 GHz (b) 2.45 GHz (c) 5.8 GHz. Figure 21. Simulated average SAR distribution on the cuboid phantom: at (a) 1.8 GHz (b) 2.45 GHz (c) 5.8 GHz. Figure 22. Link margin between Tx (proposed ant.) and Rx (monopole ant.) antennas at 1.8/2.45/5.8 GHz frequency bands. Figure 22. Link margin between Tx (proposed ant.) and Rx (monopole ant.) antennas at 1.8/2.45/5.8 GHz frequency bands. Table 1. Proposed antenna and previously reported textile antennas. Table 1. Proposed antenna and previously reported textile antennas. Ref. (Year)[19](2020)[20](2021)[21](2022)[22](2022)[23](2023)This WorkArea(mm2)65 × 6060 × 6060 × 6055 × 4084 × 6960 × 60Area(λ02)0.18 × 0.17(0.03)0.49 × 0.49(0.24)0.64 × 0.64(0.41)1.46 × 1.06(1.55)0.55 × 0.67(0.37)0.36 × 0.36(0.13)Frequency (GHz)0.868/2.452.45/3.452.4/3.32/3.93/5.882.4/51.8/2.45/5.8B.W. (%)NG/3.54.9/6.73.7/5.7/5.85/9.813.15/7617.2/39.1/19.6Peak gain (dBi)NG/−1.46.7/8.9−0.81/−2.81/−1.16/2.85.27.23.7/5.3/9.6SAR (W/Kg)1 gm/10 gmNG0.1/0.04(at 0.5 W)0.11/0.33(at 1 W)0.7/---(at 1 W)NG0.0796/0.07590.0575/0.05520.0226/0.0204(at 1 W) Table 2. Antenna’s design parameters (in mm). Table 2. Antenna’s design parameters (in mm). SymbolValueSymbolValueSymbolValueSymbolValueL60L718WF3.6X118.5LP50L813W1–W66.0X234.5LF15L918W705X321.0L125L1012W811X417.0L209L113.0W903X57.5L303L1208W1011Y14.0L407L1338W1103Y2–Y45.0L503W60W1206 L63.5WP40W1331 Table 3. Boresight peak gain values (dBi). Table 3. Boresight peak gain values (dBi). Frequency(GHz)Simulation(Chest Phantom)Measured(on Human Chest)1.83.72.82.455.34.65.89.68.2 Table 4. Boresight peak gain values (dBi) at different bending radii: 45 mm, 35 mm, and 25 mm. Table 4. Boresight peak gain values (dBi) at different bending radii: 45 mm, 35 mm, and 25 mm. Frequency (GHz)At 45 mmAt 35 mmAt 25 mm1.82.12.00.2 2.454.54.63.25.88.28.17.8 Table 5. Maximum SAR of the proposed antenna (at 1 W input power). Table 5. Maximum SAR of the proposed antenna (at 1 W input power). Frequency(GHz)Maximum SAR (on Phantom)1 gm10 gm1.80.07960.07592.450.05750.05525.80.02260.0204 Table 6. Link budget parameters. Table 6. Link budget parameters. Transmitter Frequency (GHz)1.8/2.45/5.8GtAntenna gain (dBi)3.7/5.3/9.6PtTransmitted power (dBm)16 EIRP (dBm)19.7/21.3/25.6ReceiverGrReceiver antenna gain (dBi)(external antenna)2.15ToAmbient temperature (K)293 Boltzmann constant1.38 × 10−23NoNoise power density (dB/Hz)−203.9Signal qualityBrBit rate (Mbps)0.250, 1, 10 Eb/NoIdeal PSK (dB)9.6GcCoding gain (dB)0GdFixing deterioration (dB)2.5 Disclaimer/Publisher’s Note: The statements, opinions and data contained in
2025-04-20137, 104301. [Google Scholar] [CrossRef]Zhang, K.Y.; Wang, Y.; Ai, Y.B. Analytical solution to interaction between pipelines and soils under arbitrary loads. Chin. J. Geotech. Eng. 2010, 32, 1189–1193. (In Chinese) [Google Scholar]Zhao, M.; Xu, L.; Huang, J.; Du, X.; Li, H. Analytical solutions of the tunnels under the fault creeping by elastic foundation beam model with considering tangential interaction. Soil Dyn. Earthq. Eng. 2023, 172, 108047. [Google Scholar] [CrossRef] Figure 1. Displacement of the free field. Figure 1. Displacement of the free field. Figure 2. Euler beam on the Winkler foundation. Figure 2. Euler beam on the Winkler foundation. Figure 3. A double cosine load applied on the plane xoy. Figure 3. A double cosine load applied on the plane xoy. Figure 4. A simple cosine load acting on a foundation. Figure 4. A simple cosine load acting on a foundation. Figure 5. Displacement coordination of the beam and ground. Figure 5. Displacement coordination of the beam and ground. Figure 6. Three-dimensional solid finite element model. Figure 6. Three-dimensional solid finite element model. Figure 7. Beam–spring numerical model. Figure 7. Beam–spring numerical model. Figure 8. Beam displacement along the axis obtained via different methods [20]. Figure 8. Beam displacement along the axis obtained via different methods [20]. Figure 9. Beam internal forces along the axis obtained using different methods (a) bending moment; (b) shear force [20]. Figure 9. Beam internal forces along the axis obtained using different methods (a) bending moment; (b) shear force [20]. Figure 10. The errors of the tunnel’s peak internal forces along the axis using different elastic moduli: (a) bending moment; (b) shear force [20]. Figure 10. The errors of the tunnel’s peak internal forces along the axis using different elastic moduli: (a) bending moment; (b) shear force [20]. Table 1. Fitting data from the two
2025-03-25DimensionalD. Perpendicular on OC (produced) from point object, e.g., a ring, a disc, any plane sheet, etc.D is DN. Moment of inertia of the object about N³the axis ACB is IC (DC)2 dm , and about Mthe axis MOP it is IO ³ DO 2 dm . ? IO ³ DO 2 dm ³ >DN@2 >NO@2 dm³ >DN@2 [NC]2 2.NC.CO >CO@2 dm Fig. 1.16: Theorem of perpendicular axes. 15Figure 1.16 shows a rigid laminar object able (II) Consider any two mutually perpendicularto rotate about three mutually perpendicularaxes x, y and z. Axes x and y are in the plane diameters x and y of the flywheel. If theof the object while the z axis is perpendicularto it, and all are concurrent at O. Consider a flywheel rotates about these diameters, thesemass element dm located at any point P. PM= y and PN = x are the perpendiculars drown three axes (own axis and two diameters) willfrom P respectively on the x and y axes. Therespective perpendicular distances of point be mutually perpendicular and concurrent.M from x, y and z axes will then be y, x and Thus, perpendicular axes theorem is y 2 + x2 . If Ix, Iy and Iz are the respectivemoment of inertias of the body about x, y and applicable. Let Id be the moment of inertiaz axes, we can write, of the flywheel, when rotating about its ³ ³? I x y 2dm, I y x2dm and diameter. ? Id I x I y Thus, according to the theorem of ³Iz y2 x2 dm perpendicular axes, 1 MR2 Iz 2 Ix Iy 2Id ? Id 1 MR2 4³ ³? I z y 2dm x2dm I x I yThis is the mathematical form of thetheorem of perpendicular axes. As the diameter passes through the centre It states that, “The moment of inertia of mass of the (uniform) disc, Id = IC(Iz) of a laminar object about an axis (z) Consider a tangent in the plane of the discperpendicular to its plane is the sum of itsmoment of inertias about two mutuallyperpendicular axes (x and y) in its plane, allthe three axes being concurrent”.Example 1.7: A flywheel is a mechanical and parallel to this diameter. It is at thedevice specifically designed to efficiently distance h = R from the diameter. Thus,store rotational energy. For a particular parallel axes theorem is applicable aboutmachine it is in the form of a uniform 20 kg these two axes.disc of diameter 50 cm, able to rotate about ∴ IT, parallel = Io = Ic + Mh2 = Id + MR2its own axis. Calculate its kinetic energy = 1 MR2 + MR2 = 5 MR2when rotating at 1200 rpm. Use S 2 10. 4 4Calculate its moment of inertia, in case it is 5 5 4 4rotated about a tangent in its plane. ∴ IT, parallel = MR2 = 20 × 0.252Solution: (I) As the flywheel is in the form = 1.5625 kg m2of a uniform disc rotating about its own 1.8
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