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Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Mo = 2.3 14° A1 10° A2 A 2D external-compression supersonic inlet designed for a flight Mach number of 2.3 has a first compression ramp at 10 deg and a second ramp at 14 deg additional deflection. Thus the inlet shock system has two external oblique shocks with a normal shock at the inlet throat. There is a subsonic diffusion section downstream of the normal shock with area ratio A2/A1 = 1.22 For this inlet at its design condition determine the following: a) Inlet total pressure recovery Pt2/Pto based on shock losses b) Mach number at the engine face M2 Assume isentropic flow in the subsonic diffuser section with y = 1.4
Transcribed Image Text:Mo = 2.3 14° A1 10° A2 A 2D external-compression supersonic inlet designed for a flight Mach number of 2.3 has a first compression ramp at 10 deg and a second ramp at 14 deg additional deflection. Thus the inlet shock system has two external oblique shocks with a normal shock at the inlet throat. There is a subsonic diffusion section downstream of the normal shock with area ratio A2/A1 = 1.22 For this inlet at its design condition determine the following: a) Inlet total pressure recovery Pt2/Pto based on shock losses b) Mach number at the engine face M2 Assume isentropic flow in the subsonic diffuser section with y = 1.4
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