This document provides information about the design of a roof structure including:
1. Load calculations for dead loads from roofing materials and live loads from rain and workers.
2. Load factors are applied to calculate design loads.
3. Moment and shear force calculations are performed based on the design loads.
4. Steel I-beam profiles are selected to resist the maximum tensile and compressive forces calculated.
5. The profiles are checked against design strength limits for yielding, ultimate strength, and block shear.
Base plate biasanya terdapat pada ujung kolom baja. Untuk mengetahui ketebalan dan jumlah baut yang digunakan pada base plate maka digunakanlah metode excel untuk mengetahui baseplate yang dapat memikul beban yang disalurkan kolom
Base plate biasanya terdapat pada ujung kolom baja. Untuk mengetahui ketebalan dan jumlah baut yang digunakan pada base plate maka digunakanlah metode excel untuk mengetahui baseplate yang dapat memikul beban yang disalurkan kolom
Perancangan struktur kuda kuda baja tipe gableAfret Nobel
Perancangan struktur kuda kuda baja tipe gable adalah laporan mengenai perencanaan struktur bangunan gudang dengan struktur baja gable sebagai struktur utama.
Perancangan struktur kuda kuda baja tipe gableAfret Nobel
Perancangan struktur kuda kuda baja tipe gable adalah laporan mengenai perencanaan struktur bangunan gudang dengan struktur baja gable sebagai struktur utama.
Analisis struktur gedung bertingkat rendah dengan software etabs v9Afret Nobel
Analisis struktur gedung bertingkat rendah dengan software etabs v9. Menjelaskan langkah-langkah prosedur mendesain bangunan bertingkat menggunakan software ETABS.
Roof Truss Design (By Hamza Waheed UET Lahore )Hamza Waheed
This presentation defines, describes and presents the most effective and easy way to design a roof truss with all the necessary steps and calculations based on Allowable Stress Design. Soft-wares like MD Solids, Truss Analysis have been used. It is most convenient way to design a roof truss which is being the most important structural components of All types of steel bridges.
Explains in detail about the planning and designing of a G + 2 school building both manually and using software (STAAD Pro).
With the reference with this we could design a building of a school with 2 blocks and G + 2 building.
Overview of the fundamental roles in Hydropower generation and the components involved in wider Electrical Engineering.
This paper presents the design and construction of hydroelectric dams from the hydrologist’s survey of the valley before construction, all aspects and involved disciplines, fluid dynamics, structural engineering, generation and mains frequency regulation to the very transmission of power through the network in the United Kingdom.
Author: Robbie Edward Sayers
Collaborators and co editors: Charlie Sims and Connor Healey.
(C) 2024 Robbie E. Sayers
NUMERICAL SIMULATIONS OF HEAT AND MASS TRANSFER IN CONDENSING HEAT EXCHANGERS...ssuser7dcef0
Power plants release a large amount of water vapor into the
atmosphere through the stack. The flue gas can be a potential
source for obtaining much needed cooling water for a power
plant. If a power plant could recover and reuse a portion of this
moisture, it could reduce its total cooling water intake
requirement. One of the most practical way to recover water
from flue gas is to use a condensing heat exchanger. The power
plant could also recover latent heat due to condensation as well
as sensible heat due to lowering the flue gas exit temperature.
Additionally, harmful acids released from the stack can be
reduced in a condensing heat exchanger by acid condensation. reduced in a condensing heat exchanger by acid condensation.
Condensation of vapors in flue gas is a complicated
phenomenon since heat and mass transfer of water vapor and
various acids simultaneously occur in the presence of noncondensable
gases such as nitrogen and oxygen. Design of a
condenser depends on the knowledge and understanding of the
heat and mass transfer processes. A computer program for
numerical simulations of water (H2O) and sulfuric acid (H2SO4)
condensation in a flue gas condensing heat exchanger was
developed using MATLAB. Governing equations based on
mass and energy balances for the system were derived to
predict variables such as flue gas exit temperature, cooling
water outlet temperature, mole fraction and condensation rates
of water and sulfuric acid vapors. The equations were solved
using an iterative solution technique with calculations of heat
and mass transfer coefficients and physical properties.
We have compiled the most important slides from each speaker's presentation. This year’s compilation, available for free, captures the key insights and contributions shared during the DfMAy 2024 conference.
Cosmetic shop management system project report.pdfKamal Acharya
Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
Contact with Dawood Bhai Just call on +92322-6382012 and we'll help you. We'll solve all your problems within 12 to 24 hours and with 101% guarantee and with astrology systematic. If you want to take any personal or professional advice then also you can call us on +92322-6382012 , ONLINE LOVE PROBLEM & Other all types of Daily Life Problem's.Then CALL or WHATSAPP us on +92322-6382012 and Get all these problems solutions here by Amil Baba DAWOOD BANGALI
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About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
CW RADAR, FMCW RADAR, FMCW ALTIMETER, AND THEIR PARAMETERSveerababupersonal22
It consists of cw radar and fmcw radar ,range measurement,if amplifier and fmcw altimeterThe CW radar operates using continuous wave transmission, while the FMCW radar employs frequency-modulated continuous wave technology. Range measurement is a crucial aspect of radar systems, providing information about the distance to a target. The IF amplifier plays a key role in signal processing, amplifying intermediate frequency signals for further analysis. The FMCW altimeter utilizes frequency-modulated continuous wave technology to accurately measure altitude above a reference point.
Hierarchical Digital Twin of a Naval Power SystemKerry Sado
A hierarchical digital twin of a Naval DC power system has been developed and experimentally verified. Similar to other state-of-the-art digital twins, this technology creates a digital replica of the physical system executed in real-time or faster, which can modify hardware controls. However, its advantage stems from distributing computational efforts by utilizing a hierarchical structure composed of lower-level digital twin blocks and a higher-level system digital twin. Each digital twin block is associated with a physical subsystem of the hardware and communicates with a singular system digital twin, which creates a system-level response. By extracting information from each level of the hierarchy, power system controls of the hardware were reconfigured autonomously. This hierarchical digital twin development offers several advantages over other digital twins, particularly in the field of naval power systems. The hierarchical structure allows for greater computational efficiency and scalability while the ability to autonomously reconfigure hardware controls offers increased flexibility and responsiveness. The hierarchical decomposition and models utilized were well aligned with the physical twin, as indicated by the maximum deviations between the developed digital twin hierarchy and the hardware.
Gen AI Study Jams _ For the GDSC Leads in India.pdf
Baja kuda kuda
1. Nama : Vicky Wildan Y Dosen Pembimbing : Dr.Nindyawati, S.T., M.T.
NIM : 120523417699
Offering :
A. DATA ATAP
Jenis atap = Genteng
Berat = 50 kg/m²
Plafon = 30 kg/m²
Angin (dari tepi laut, PPI : 22) = 25 kg/m²
Angin Tekan 0,02*α - 0,4*s*Tek.Angin*Jarak.kuda-kuda*jarak Gording = 30.00 kg/m²
Angin Hisap -0,4*s*tek.angin*Jarak.kuda-kuda*jarak Gording = -120.00 kg/m²
B. DATA BAHAN
Tegangan leleh baja (yield stress) fy = 250 MPa BJ41
Tegangan tarik putus (ultimate stress) fu = 410 MPa
Tegangan sisa (residual stress) fr = 70 MPa
Modulus elastik baja (modulus of elasticity) E = 200000 MPa
Angka Poisson (Poisson's ratio) ʋ = 0.3
SNI-03-1729-2002 5.1.3 hal 29
C. DATA PROFIL BAJA
Profil : Double L - Sama Kaki 90x90x10
H = 90 mm
B = 90 mm
t = 10 mm
r1 = 10 mm
r2 = 7 mm
A = 1700 mm²
Ix = 1250000 mm⁴
Iy = 1990000 mm⁴
Sx = Sy = 19500 mm³
rx=ry = 27.1 mm
r-max = 34.2 mm
r-min = 17.4 mm
Berat profil w = 13.3 kg/m
Gambar 1. Profil IWF (PT. Gunung Garuda)
E. DATA KUDA-KUDA
Panjang elemen thd. Sb x L = 11892.30 mm
Momen Maksimum akibat bebn terfaktor Mu = 4101274.6 mm
Momen Pada 1/4 bentang Ma = 1025318.7 mm
Momen ditengah bentang Mb = 4101274.6 mm
Momen Pada 3/4 bentang Mc = 1025318.7 mm
Gaya geser akibat beban terfaktor Vu = 9906.7764 mm
Faktor reduksi kekuatan untuk lentur φb = 0.9 mm
Faktor reduksi kekuatan untuk geser φf = 0.75 mm
F. SECTION PROPERTY
G = E / [ 2 x ( 1 + ʋ ) ] = 76923.077 MPa
h1 = tf + r = 17 mm
h2 = ht - 2 * h1 = 56 mm
h = ht - tf = 80 mm
J = Ʃ*b x t
3
/3] = 2 x 1/3 x bf x tf³ + 1/3 x ( ht - 2 x tf ) x tw³ = 8.33E+04 mm⁴
Iw = Iy x h² / 4 = 3.184E+09 mm⁶
X1 = π / Sx x √ [ E x G x J x A / 2 ] = 1.68E+05 MPa
X2 = 4 x [ Sx / ( G x J ) ]² x Iw / Iy = 5.922E-08 mm²/N²
Zx = tw x ht²/4 + (bf - tw) x ( ht - tf ) x tf = 84250 mm²
Zy = tf x bf²/2 + (ht - 2 x tf) x tw²/4 = 42250 mm²
G = modulus geser Zx = modulus penampang plastis terhadap sb x
J = konstanta puntir torsi Zy = modulus penampang plastis terhadap sb y
Iw = konstanta puntir lengkung X1 = koefisien momen tekuk torsi lateral -1,
h = tinggi bersih badan X2 = koefisien momen tekuk torsi lateral - 2,
Atap
PERHITUNGAN KUDA-KUDA
2. Lebar Q 1600 0.01
(m) (N/m) 16
1 Beban Gording 83.2 N/m 4.00 332.8
Beban Atap 500 N/m² 15.59 649.5191
Berat plafond 300 N/m² 300
1282.319
Beban Sambungan (10%) 10% 1282.319053 128.2319
Beban Aksessories (10%) 10% 128.2319053 12.82319
1423.374
Gambar 2. Beban Mati (Staad Pro 2004)
2.2 BEBAN HIDUP (LIVE LOAD)
Jarak antara gording s = 2 m
Beban air hujan q hujan x s x 10³ = 500 N/m
Beban hidup merata akibat air hujan QLL = 500 N/m
Beban hidup terpusat akibat beban pekerja (PPI:22) 100 Kg PLL = 1000 N
Gambar 3. Beban Hidup(Staad Pro 2004)
2. BEBAN PADA KUDA-KUDA (PPIUG 1983)
0.25 kN/m²
No Material Berat Satuan
Beban hidup akibat beban air hujan diperhitungkan setara dengan beban genangan air setebal
1 inc = 25 mm
q hujan = 0,025 x 10 =
Jumlah
2.1 BEBAN MATI (DEAD LOAD)
Jumlah Total
3. 2.3 BEBAN ANGIN (WIND LOAD)
1 300 N/m²
2 -1200 N/m²
Gambar 4. Angin Tekan dan Angin Hisap(Staad Pro 2004)
3. BEBAN TERFAKTOR (SNI 03-1729-2002 PASAL 6.2.2)
Beban merata Qu = 1,2 x QDL + 1,6 x QLL+ 0,8W = 2748.049 N/m
Beban terpusat Pu = 1,6 x PLL = 1600 N
Sudut miring atap α = 0.480 deg
Beban merata Qu = Qu x 10
-
³ = 2.748 N/m
Beban terpusat Pu = Pu x cos α = 768 N
Angin Tekan
Angin Hisap
Beban Angin Pada Atap
No Jenis Angin Berat Satuan
4. 4. MOMEN DAN GAYA GESER AKIBAT BEBAN TERFAKTOR
Panjang bentang Kuda kuda sumbu lokal L = L1 = 10392.30 mm
Momen akibat beban terfaktor terhadap sumbu lokal Mux = 1/10 x Qux x Lx² + 1/8 x Pux x Lx = 30676590 Nmm
Momen pada 1/4 bentang MA = 3/4*Mux = 23007443 Nmm
Momen di tengah bentang MB = Mux = 30676590 Nmm
Momen pada 3/4 bentang MC = 3/4*Mux = 23007443 Nmm
Gambar 5. Reaksi Perletakan
Perhitungan Gaya Batang
Beam L/C Axial Force N
Tekan (-) Tarik (+)
13 4 -93129.9
4 4 87845
14 4 87267.3
12 4 -82775.3
12 4 -82775.3
27 4 -79383.3
3 4 75333.4
26 4 -72881.1
11 4 -72105.5
18 4 69818
25 4 -65727.3
15 4 63064.2
17 4 62222.1
17 4 62222.1
10 4 -61470.5
24 4 -58571
29 4 54305.1
19 4 -51336.9
5 4 -50821.3
2 4 50750.6
16 4 46273.8
1 4 45449.6
30 4 -18133.2
31 4 -15401.3
32 4 -13208
6 4 12674.3
33 4 -11581.8
34 4 -11561.8
35 4 -10012.7
7 4 8698.7
36 4 -8528
20 4 8275.7
37 4 -7228.3
21 4 5599.8
8 4 4753.7
22 4 3010.2
23 4 -111.5
9 4 100.6
-93129.9 87845
RA 29932.4
RB 26332.4
Nilai Maksimum
5. 5. PERENCANAAN PROFIL
5.1 Batang tarik
Dimensi Profil
Profil Siku 90 x 90 x 10
H = 90 mm
B = 90 mm
t = 10 mm
r1 = 10 mm
r2 = 7 mm
A = 1700 mm²
Ix = 1250000 mm´
Iy = 1990000 mm´
Sx = Sy = 19500 mm³
rx=ry = 27.1 mm
r-max = 34.2 mm
r-min = 17.4 mm
w = 13.3 kg/m
Batang Tarik Maksimum = 87845 N
Panjang Batang Tarik Maks = 2.13 m
фbaut = 12 mm
фlubang SNI 03-1729-2002, Diameter Lubang < 24mm = фbaut + 2mm = 14 mm
Kontrol Kelangsingan Struktur Tarik
Jari Jari Girasi (digunakan r min) r-min = 1.74 cm
Panjang Batang L = 213 cm
Kelangsingan λ = L/r = 122.41 cm
Tahanan Nominal
Batas Leleh Faktor Tahanan (tegangan leleh) φ = 0.9
Batas Leleh Pu = f. fy.Ag = 382500
Periksa Batas Leleh
382500 > 87845 (OK)
Batas Putus
Kondisi Fraktur Faktor Tahanan fraktur) φ = 0.75
Luas Neto An = Ag - фlubang * t atau An<0.85*Ag = 1445 mm2
Koef reduksi U = 1 - x/L = 0.84
Luas Penampang Efektif Ae = U * An = 1212.99 mm
2
Kondisi Putus (Fraktur) Pu = φ*fu*Ae = 372993.2 N
Periksa Kondisi Putus (Fraktur )
372993 > 87845 (OK)
Kontrol Geser Blok (Block Shear )
Luas Neto Akibat Geser (ditinjau 100 mm) Anv = 100*t*2-(фlubang*2) = 1972 mm2
Luas Neto Akibat Tarik (ditinjau 100 mm) Ant = H*t*2-(фlubang*2) = 1772 mm
2
fu . Ant 0.6.Fu.Anv
726520 > 485112
Maka Tn = 0.6*fy*Agv+fu*Ant
Luas Bruto Akibat Geser (ditinjau 100 mm) Agv = 100*t*2 = 2000 mm
2
Tahanan Nominal Tn = 0.6*fy*Agv+fu*Ant = 1026520 mm2
Periksa Batas Leleh
1026520 > 87845 (OK)
6. 5.2 Batang Tekan
Batang Tekan Maksimum = -93129.9 N
Panjang Batang Tarik Maks = 2.39 m
фbaut = 12 mm
фlubang SNI 03-1729-2002, Diameter Lubang < 24mm = фbaut + 2mm = 14 mm
Periksa Kestabilan Elemen
Flens
Syarat λ = b/t ≤ 200/(fy)^0.5
9 < 12.649 (OK)
Web tidak ada syarat untuk profil siku
Kapasitas Profil
Mu = f Mn
Kondisi Tumpuan pada Batang = Sendi - sendi
Faktor Panjang Tekuk k = 1
λ = k*L/r = 88.19
λc = λ/π*fy/E)^0.5 = 0.99
Syarat 0.25 < λc < 1.2
0.25 < 0.99 < 1.2
ω = 1.43/(1.6-0.67λc) = 1.34
Nn = Ag*fcr = Ag*fy/ω = 317766.2 N
Nu/ф*Nn = 0.010174
Syarat 0.010174143 < 1
maka Dimensi Profil Kuat Memikul Beban Terfaktor
SNI 03-1729-2002 (LRFD;62)