1 / 24

Antennas and open-frame structures

Antennas and open-frame structures. Wind loading and structural response Lecture 23 Dr. J.D. Holmes. Antennas and open-frame structures. Antennas - isolated structures - radio telescopes and microwave antennas. Antennas - attached to towers - aerodynamic interference. Single frames.

Samuel
Télécharger la présentation

Antennas and open-frame structures

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Antennas and open-frame structures Wind loading and structural response Lecture 23 Dr. J.D. Holmes

  2. Antennas and open-frame structures • Antennas - isolated structures - radio telescopes and microwave antennas • Antennas - attached to towers - aerodynamic interference • Single frames • Multiple frames • Lattice towers Common feature : aerodynamic interference between various elements - e.g. antennas and supporting tower or other antennas, members of a frame

  3. f Focus Antennas and open-frame structures • Radio telescope • Paraboloid dish

  4. 2f Approximate center of aerodynamic forces d C e Antennas and open-frame structures • Radio telescope • Paraboloid dish Normal to dish surface intersects axis at 2  focal length

  5. FY d FX e  b Wind Antennas and open-frame structures • Radio telescope • Paraboloid dish Fy force generates significant moments about dish supports

  6. Focus 0.10 0.08 0.06 0.04 0.02 0 Total moment Azimuth angle, 135o Effect of boundary layer profile Zenith angle b Altitude moment CM Azimuth moment Wind Altitude axis Azimuth angle 0 20 40 60 80 90 Zenith angle, degrees a PLAN VIEW Antennas and open-frame structures • Radio telescope • Paraboloid dish

  7. 2.0 1.5 b  1.0 0.5 1% turbulence 10% turbulence 0.0 120 140 160 0 40 60 180 80 100 20  (degrees) Antennas and open-frame structures • Microwave dish antenna • Impermeable dish A = (b2/4) (projected area) Small effect of turbulence

  8. Da WIND Dt WIND De WIND Antennas and open-frame structures • Microwave dish antenna • Interference factor

  9. Experimental data Equation with t=0.5 1.5 1 Interference factor 0.5 0 0 45 90 135 180 Wind direction (degrees) Antennas and open-frame structures • Microwave dish antenna • Interference factor Ki = exp [-k(CD)2]. [(1+t) + t cos 2( - d - 90)]

  10. Cd (ref.b)  0.8 Cd1.1 120O b Antennas and open-frame structures • Cell-phone antenna • isolated panels

  11. combined Cd (ref.b)  1.1 combined Cd (ref.b)  0.9 ~2b Antennas and open-frame structures • Cell-phone antenna • grouped panels grouping gives large reduction in total drag

  12. 60o 0o Antennas and open-frame structures • Cell-phone antenna • grouped panels total drag of group : about 30% less than sum of individual elements

  13. 2.0 CD 1.0 0 0.5 1.0 Solidity ratio, Antennas and open-frame structures • Open frames • Single frame. Two-dimensional. Normal wind • sharp-edged members solidity = ‘solid’ area of frame/total enclosed area reference area for drag coefficient = ‘solid’ area of frame drag coefficient relatively independent of details of member arrangement

  14. 2.0 CD 1.0 0 0.5 1.0 Solidity ratio,  Antennas and open-frame structures • Open frames • Single frame. Two-dimensional. Normal wind at low solidity, members act as individual elements at high solidity, frame acts as a solid plate (Lecture 8) intermediate solidity : aerodynamic interference between members CD 1.6

  15. b s approximately, 1  1, Antennas and open-frame structures • Open frames • Pairs of frames. Two-dimensional. Normal wind CD(2) = CD(1) [ 1 + 2] 1 CD(1) is drag coefficient of upstream frame (downstream frame influences upstream frame) 2 CD(1) is drag coefficient of downstream frame 0 <  < 0.5 For circular members, equivalent solidity to calculate 2 , e  1.2 1.75

  16. spacing/width = 1.0 spacing/width = 0.1 15 75 angle of attack,  Antennas and open-frame structures • Open frames • 3 frames in series. Solidity = 0.1 X() = force normal to frame A = projected area of one frame at 0o angle of attack

  17. spacing/width = 1.0 spacing/width = 0.1 15 75 angle of attack,  Antennas and open-frame structures • Open frames • 3 frames in series. Solidity = 0.5 A = projected area of one frame at 0o angle of attack Maximum CXN at 30o to 45o

  18. spacing/width = 1.0 spacing/width = 0.1 15 75 angle of attack,  Antennas and open-frame structures • Open frames • 10 frames in series. Solidity = 0.1 A = projected area of one frame at 0o angle of attack

  19. spacing/width = 1.0 spacing/width = 0.1 15 75 angle of attack,  Antennas and open-frame structures • Open frames • 10 frames in series. Solidity = 0.5 A = projected area of one frame at 0o angle of attack Maximum CXN at 30o to 45o

  20. Antennas and open-frame structures • Open frames • Design method : • ‘Wind loads and anchor bolt design for petrochemical facilities’ (ASCE) Needs more wind tunnel studies for pipe racks etc.

  21. 4.0 3.5 3.0 2.5 2.0 1.5 Drag coefficient CD (q=0O) Australian Standards 0.0 0.2 0.4 0.6 0.8 1.0 Solidity Ratiod Antennas and open-frame structures • Drag coefficients for lattice tower (Lecture 21) Square cross section with flat-sided members (wind normal to face) CD = 4.2 - 7 (for 0.1< < 0.2) CD = 3.5 - 3.5 (for 0.2< < 0.5) (ASCE-7 : CD = 4.02 – 5.9 +4.0 )  = solidity of one face = area of members  total enclosed area includes interference and shielding effects between members

  22. Antennas and open-frame structures • Drag coefficients for lattice tower Triangular cross section with flat-sided members CD = 3.5 - 4 (for 0.1< < 0.3) CD = 2.9 – 2 (for 0.3<  < 0.5) (ASCE-7 : CD = 3.42 – 4.7 +3.4 )

  23. Antennas and open-frame structures • Drag coefficients for lattice tower Cross section with circular members depends on Reynolds Number for super-critical flow - Cd for cross section ~ 0.5 times that for equivalent sharp-edged tower with same solidity some members may be in super-critical flow - others in sub-critical flow

  24. End of Lecture 23John Holmes225-405-3789 JHolmes@lsu.edu

More Related