EBK MUNSON, YOUNG AND OKIISHI'S FUNDAME
8th Edition
ISBN: 9781119547990
Author: HOCHSTEIN
Publisher: JOHN WILEY+SONS INC.
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Chapter 11.6, Problem 36P
(a)
To determine
The air speed and the Mach number if flow is incompressible.
(b)
To determine
The air speed and the Mach number if flow is compressible.
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A continuous column flash system is separating 100 kmol/h of a saturated liquid feed that is 45 mol% methanol and 55 mol% water at 1.0 atm. Operate with L/V = 1.5 and the outlet bottoms at xN = 0.28.
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Chapter 11 Solutions
EBK MUNSON, YOUNG AND OKIISHI'S FUNDAME
Ch. 11.1 - Prob. 1PCh. 11.1 - Air flows steadily between two sections in a duct....Ch. 11.1 - Consider the flow process in Fig. P11.3. Does the...Ch. 11.1 - Prob. 4PCh. 11.1 - Prob. 5PCh. 11.1 - Prob. 6PCh. 11.1 - Prob. 7PCh. 11.1 - Prob. 8PCh. 11.1 - Air flows in a 15-cm-diameter horizontal pipe. At...Ch. 11.1 - An air heater in a large coal-fired steam...
Ch. 11.2 - Determine the static pressure to stagnation...Ch. 11.2 - Prob. 12PCh. 11.2 - Prob. 13PCh. 11.2 - Prob. 14PCh. 11.2 - Prob. 15PCh. 11.3 - Prob. 16PCh. 11.3 - Prob. 17PCh. 11.3 - Prob. 18PCh. 11.3 - Prob. 19PCh. 11.3 - Prob. 20PCh. 11.3 - Prob. 21PCh. 11.3 - Prob. 22PCh. 11.4 - Prob. 23PCh. 11.4 - Prob. 24PCh. 11.4 - Prob. 25PCh. 11.4 - Prob. 26PCh. 11.4 - Prob. 27PCh. 11.4 - Air flows in a constant-area, insulated duct. The...Ch. 11.5 - Prob. 29PCh. 11.5 - The Pitot tube on a supersonic aircraft (see Video...Ch. 11.5 - An aircraft cruises at a Mach number of 2.0 at an...Ch. 11.5 - Prob. 32PCh. 11.5 - Prob. 33PCh. 11.5 - Prob. 34PCh. 11.5 - Prob. 35PCh. 11.6 - The stagnation pressure and temperature of air...Ch. 11.6 - Prob. 37PCh. 11.6 - Prob. 38PCh. 11.6 - Prob. 39PCh. 11.6 - Prob. 40PCh. 11.6 - Prob. 41PCh. 11.6 - The static pressure to stagnation pressure ratio...Ch. 11.7 - Air flows steadily and isentropically from...Ch. 11.7 - Prob. 44PCh. 11.7 - Prob. 45PCh. 11.7 - Prob. 46PCh. 11.7 - At a certain point in a pipe, air flows steadily...Ch. 11.7 - Prob. 48PCh. 11.7 - Prob. 49PCh. 11.7 - Prob. 50PCh. 11.7 - A jet engine is to be designed for an altitude of...Ch. 11.7 - Prob. 52PCh. 11.7 -
A convergent–divergent nozzle has an exit throat...Ch. 11.7 - An ideal gas flows isentropically through a...Ch. 11.8 - Standard atmospheric air (T0 = 59 F, p0 = 14.7...Ch. 11.8 - Prob. 57PCh. 11.8 - Prob. 58PCh. 11.8 - Prob. 59PCh. 11.8 - Prob. 64PCh. 11.9 - Prob. 66PCh. 11.9 - Prob. 67PCh. 11.9 - Prob. 68PCh. 11.9 - Air enters a frictionless, constant area duct with...Ch. 11.9 - Prob. 70PCh. 11.9 - Prob. 71PCh. 11.9 - Prob. 72PCh. 11.9 - Prob. 73P
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Intro to Compressible Flows — Lesson 1; Author: Ansys Learning;https://www.youtube.com/watch?v=OgR6j8TzA5Y;License: Standard Youtube License