Combustion Ma >1 Ma >1 4

Refrigeration and Air Conditioning Technology (MindTap Course List)
8th Edition
ISBN:9781305578296
Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Chapter39: Residential Energy Auditing
Section: Chapter Questions
Problem 14RQ: Briefly describe and write the equation for incomplete combustion.
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Engineers call the supersonic combustion in a scramjet
engine almost miraculous, “like lighting a match in a hurricane.”
Figure C9.8 is a crude idealization of the engine.
Air enters, burns fuel in the narrow section, then exits, all at supersonic speeds. There are no shock waves. Assume areas
of 1 m2 at sections 1 and 4 and 0.2 m2 at sections 2 and
3. Let the entrance conditions be Ma1 = 6, at 10,000 m
standard altitude. Assume isentropic fl ow from 1 to 2,
frictionless heat transfer from 2 to 3 with Q = 500 kJ/kg,
and isentropic fl ow from 3 to 4. Calculate the exit conditions
and the thrust produced.

Combustion
Ma >1
Ma >1
4
Transcribed Image Text:Combustion Ma >1 Ma >1 4
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