MindTap Engineering for Dunlap's Sustainable Energy, SI Edition, 2nd Edition [Instant Access], 1 term (6 months)
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Chapter 3, Problem 15P
To determine

Find the volume of fuel needed to accelerate the ship from rest to cruising speed.

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A JET PLANE WHICH WEIGHT 29430 N AND HAS A WING AREA OF 20 M² FLIES AT A VELOCITY OF 250 KM/HR. WHEN THE ENGINE DELIVERS 7357.5 KW, 65% OF THE POWER IS USED TO OVERCOME THAT DRAG RESISTANCE OF THE WING. CALCULATE THE CO-EFFICIENT OF LIFT AND CO-EFFICIENT OF DRAG FOR THE WING. TAKE DENSITY OF AIR EQUAL TO 1.21 KG/M³.
Question 4 of 10 0/1 E View Policies Show Attempt History Current Attempt in Progress In a diesel engine the fuel is ignited when it is injected into hot compressed air, heated by the compression itself. In a typical high-speed diesel engine, the chamber in the cylinder has a diameter of 10.7 cm and a length of 13.4 cm. On compression, the length of the chamber is shortened by 12.7 cm (a “5-inch stroke"). The compression of the air changes its pressure from 1.00 to 39.5 atm. The temperature of the air before compression is 391 K. As a result of the compression, what will be the final air temperature (in Kand °C) just before the fuel injection? temperature = K = i °C eTextbook and Media Hint Assistance Used Determine the volume change as a way to get a handle on the new temperature. What equation relates pressure, temperature, and volume? The volume of the cylinder = z r² (height). Remember that the radius is half the diameter. Save for Later
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