My WebLink
|
Help
|
About
|
Sign Out
Home
Browse
Search
11625 AIRPORT RD SONRISE CHRISTIAN CENTER 2025-04-11
>
Address Records
>
AIRPORT RD
>
11625
>
SONRISE CHRISTIAN CENTER
>
11625 AIRPORT RD SONRISE CHRISTIAN CENTER 2025-04-11
Metadata
Thumbnails
Annotations
Entry Properties
Last modified
4/11/2025 9:58:33 AM
Creation date
3/3/2025 7:59:47 AM
Metadata
Fields
Template:
Address Document
Street Name
AIRPORT RD
Street Number
11625
Tenant Name
SONRISE CHRISTIAN CENTER
Imported From Microfiche
No
There are no annotations on this page.
Document management portal powered by Laserfiche WebLink 9 © 1998-2015
Laserfiche.
All rights reserved.
/
122
PDF
Print
Pages to print
Enter page numbers and/or page ranges separated by commas. For example, 1,3,5-12.
After downloading, print the document using a PDF reader (e.g. Adobe Reader).
View images
View plain text
Project Title: <br /> Engineer: <br /> Project ID: <br /> Project Descr: <br /> Steel Column Project File:230803_enercalc trib_210208_s2306010.ec6 <br /> LIC#:KW-06017385,Build:20.23.08.30 SOUND STRUCTURAL SOLUTIONS (c)ENERCALC INC 1983-2023 <br /> DESCRIPTION: (1-1) South <br /> Code References <br /> Calculations per AISC 360-16, IBC 2018,CBC 2019,ASCE 7-16 <br /> Load Combinations Used :ASCE 7-16 <br /> General Information <br /> Steel Section Name : Pipe8xS Overall Column Height 24.0 ft <br /> Analysis Method: Allowable Strength Top&Bottom Fixity Top Free,Bottom Fixed <br /> Steel Stress Grade Brace condition: <br /> Fy:Steel Yield 35 ksi Unbraced Length for buckling ABOUT X-X Axis=24.0 ft,K=1.0 <br /> E:Elastic Bending Modulus 29,000.0 ksi Unbraced Length for buckling ABOUT Y-Y Axis=24.0 ft,K=1.0 <br /> Applied Loads Service loads entered.Load Factors will be applied for calculations. <br /> Column self weight included : 1,041.60 Ibs*Dead Load Factor <br /> AXIAL LOADS . . . <br /> Cantilevered GluLam:Axial Load at 24.0 ft, D= 16.749,S= 32.625 k <br /> (1-1):Axial Load at 24.0 ft, D =8.855, S = 13.659 k <br /> DESIGN SUMMARY <br /> Bending&Shear Check Results <br /> PASS Max.Axial+Bending Stress Ratio = 0.4852 : 1 Maximum Load Reactions.. <br /> Load Combination +D+S Top along X-X 0.0 k <br /> Location of max.above base 0.0 ft Bottom along X-X 0.0 k <br /> At maximum location values are. .. Top along Y-Y 0.0 k <br /> Pa:Axial 72.930 k Bottom along Y-Y 0.0 k <br /> Pn/Omega:Allowablf 150.298 k <br /> Ma-x:Applied 0.0 k-ft Maximum Load Deflections... <br /> Mn-x/Omega:Allowable 54.142 k-ft Along Y-Y 0.0 in at 0.Oft above base <br /> for load combination: <br /> Ma-y:Applied 0.0 k-ft <br /> Mn-y/Omega:Allowable 54.142 k-ft Along X-X 0.0 in at 0.0ft above base <br /> for load combination: <br /> PASS Maximum Shear Stress Rath 0,0 : 1 <br /> Load Combination 0.0 <br /> Location of max.above base 0.0 ft <br /> At maximum location values are.. . <br /> Va:Applied 0.0 k <br /> Vn/Omega:Allowable 0.0 k <br /> Load Combination Results <br /> Maximum Axial+Bending Stress Ratios Maximum Shear Ratios <br /> Load Combination Stress Ratio Status Location Cbx Cby KxLx/Ry KyLy/Rx Stress Ratio Status Location <br /> D Only 0.177 PASS 0.00 ft 1.00 1.00 99.65 0.00 0.000 PASS 0.00 ft <br /> +D+S 0.485 PASS 0.00 ft 1.00 1.00 99.65 0.00 0.000 PASS 0.00 ft <br /> +D+0.7505 0.408 PASS 0.00 ft 1.00 1.00 99.65 0.00 0.000 PASS 0.00 ft <br /> +0.60D 0.106 PASS 0.00 ft 1.00 1.00 99.65 0.00 0.000 PASS 0.00 ft <br /> Maximum Reactions Note:Only non-zero reactions are listed. <br /> Axial Reaction X-X Axis Reaction k Y-Y Axis Reaction Mx-End Moments k-ft My-End Moments <br /> Load Combination @ Base @ Base @ Top @ Base @ Top @ Base @ Top @ Base @ Top <br /> D Only 26.646 <br /> +D+S 72.930 <br /> +D+0.7505 61.359 <br /> +0.60D 15.987 <br /> S Only 46.284 <br /> Extreme Reactions <br /> Axial Reaction X-X Axis Reaction k Y-Y Axis Reaction Mx-End Moments k-ft My-End Moments <br /> Item Extreme Value @ Base @ Base @ Top @ Base @ Top @ Base @ Top @ Base @ Top <br /> Axial @ Base Maximum 72.930 <br /> Minimum 15.987 <br /> Reaction, X-X Axis Base Maximum 26.646 <br /> , , ,4°1 <br />
The URL can be used to link to this page
Your browser does not support the video tag.