Chapter 7, Problem 24QAP

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A turbine blade made of a metal alloy (k = 17 W/m-K) has a length of 5.3 cm, a perimeter of 11 cm, and a cross-sectional area of 5.13 cm². The turbine blade is exposed to hot gas from the combustion chamber at 1133°C with a convection heat transfer coefficient of 538 W/m²K. The base of the turbine blade maintains a constant temperature of 450°C and the tip is adiabatic. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Hot gas h=538 W/m²K TL E= Turbine blade k = 17 W/m-K p=11 cm, L=5.3 cm A = 5.13cm² T=450°C Determine the temperature at the tip of the turbine blade. The temperature at the tip of the turbine blade is °C.

۲/۱ : +0 تا العنوان Ч Example 5.5 The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15, 7.5" above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the Dow rises. h2023-43-115-154 Vees 2V & Pond35. sketch the diagram for them. 147% 3-inpuls RTL-NAND having Re14502 BRO Sel: VIL VBEON 0.65V VIHAVING + 1.34V VHB VIHC Vesss: 1.142V Vine: IB RO+VBES+ 640 Vec Ret 709420 IB₁ 10.3mA Ic: Vec-VCE 5-0-2 Re 45 · 10.67-A ICCE: When A&B &C. "1" Vol No 30206 When A&B &c, "o" Uok Vec5v L.S. 5.06 4.4v VIT 94+114+1.34 -3.42 V N.ML5 V N.Mu-16u T.W= 2.75 169 N.Mu VEM VL N.ML Lex-V Re 16.41A Re ± 10.6mA Pony =69mw 37 L.S >