17-86 Air enters a normal shock at 22.6 kPa, 217 K, and680 m/s. Calculate the stagnation pressure and Mach numberupstream of the shock, as well as pressure, temperature,velocity, Mach number, and stagnation pressure downstreamof the shock.

Assume that ;Air is an ideal gas with constant specific heats and Flow through the nozzle is steady,…

Answered: 17-86 Air enters a normal shock at 22.6…

Introduction to Chemical Engineering Thermodynamics

8th Edition

ISBN:9781259696527

Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart

Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart

Chapter1: Introduction

Section: Chapter Questions

Problem 1.1P

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17-86 Air enters a normal shock at 22.6 kPa, 217 K, and 680 m/s. Calculate the stagnation pressure and Mach number upstream of the shock, as well as pressure, temperature, velocity, Mach number, and stagnation pressure downstream of the shock.