Compute for the concrete stress in Mpa at the top fiber of the given transformed beam se M = 50 kN-m. 50 25 125 25 50 (mm) ww OC 50 mm

GG-36 IGG-36 AY G00x/00 600x/00 ( COLUMN ( COLUMN COL LC L1 L2 0.75 LC OR 0.25 L1 (GREATER GOVERNS) 0.25 L2 OR 0.25 LI SPLICE ZONE FOR (GREATER GOVERNS) GIRDER TOP BARS 0.25 L1 OR 0.75 LC 0.25 L2 0.25 L1 OR 0.25 L2 (GREATER GOVERNS) SPLICE LENGTH SEE TABLE A2 SPLICE LENGTH SEE TABLE EQ. EQ. TOP BARS AT SUPPORT EQ. EQ. CONTINUOUS WEB BARS -TOP BARS AT CANTILEVER'S DISCONTINUOUS END TOP BARS AT SUPPORT TOP BARS AT MIDSPAN TOP BARS AT MIDSPAN EQ. EQ. EQ. ED NO SPLICE SHALL BE ALLOWED 2d FROM THE FACE OF THE SUPPORT 2d Вотом BARS AT SUPPORT BOTTOM BARS AT MIDSPAN Воттом ВARS AT MIDSPAN 2d NO SPLICE SHALL BE ALLOWED 20 FROM THE FACE OF THE SUPPORT 0.165 L1 ВОТОМ ВARS AT CANTILEVER'S DISCONTINUOUS END ВОTTOМ BARS AT SUPPORT 50mm MAX. AT SUPPORT 0.165 L2 HOOP REINFORCEMENT SEE SCHEDULE HOOP REINFORCEMENT SEE SCHEDULE HOOP REINFORCEMENT SEE SCHEDULE DISCONTINUOUS FREE END CONTINUOUS END "A" OR "B" (SEE REMARKS) CONTINUOUS END "A" OR "B" (SEE REMARKS) DISCONTINUOUS END A1 Omm TYP. GG-131…

Please answer quickly! Thanks

2. According to Section 10.2.3 of AC, the maximum usable strain at extreme concrete compression fiber shall be assumed equal to a. 0.004 b. 0.005 c. 0.003 d. 0.002 e. 0.001 f. 0.008

Define the term principal stresses.

Homework -3-; Locate the centroid (x, y) of the composite area. 10 in 7.5 in C 8 in 5 in 15 in 6 in

(2) * 28" 2#8 7 14" I2.5" NWC fé=3000 psi > 2 #10 z 2 #11 I 3" Grade 60 steel &Mn = ?

Define Osterberg Load Cell.

10. The compound bar, composed of the three segments shown, is initially stress-free. Compute the stress in each material if the temperature drops 25°C. Assume that the walls do not yield and use the following data: A (mm²) a (FC) E (GPa) Bronze segment 2000 19.0 x 10- 83 Aluminum segment 1400 23.0 x 10 70 Steel segment 11.7x 10 SUMMARY OF ANSWERS s00 200 OBranze MPa - 800 mm - -500 mm- +400 mm→ MPa Oalum Osteel MPa Bronze Aluminum Steel

Question 4 A 6 KN force is applied at the free end of a wood (E = 12GPa) beam with dimensions given in Fig. Q4. Neglecting the effect of fillets and stress concentration, determine (a) the maximum compressive stress and its location at section A-A; (b) the maximum shearing stress and its location at section A-A; (c) the deflection at section A-A. 6 kN 300 mm 400 mm ΤΑ 叶 ¡A Fig. Q4 96 mm -- 12 mm 12 mm 48 mm