A supersonic diffuser a fixed geometry 417K 254 and pressure are (K, and KPA), respectively. The inlet and throat cross-sectiona 0-176 m² 0.149 m2 areas are (m² and m²), respectively. Determine: (a) The Mach number to which the inlet must be over expanded for starting. (b) The Mach number for which the inlet is designed. ч17 ху t Mt = 1 & The mass-flow-rate at when the Too-K overenpounded for Start PookPa 254 is

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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A supersonic diffuser a fixed geometry inlet is operating at sea level where the temperature
417K
2ら4
and pressure are K, and 1 kPA), respectively. The inlet and throat cross - sectional
0149 m2
areas are ( m² and m²), respectively. Determine:
O.176 m?
(a) The Mach number to which the inlet must be over expanded for starting.
(b) The Mach number for which the inlet is designed.
417K x y
G The mass- Srow-rate at When tue Too-OK
hiet is dests overrenponnled fur Start Potalk Pa
d- the mers -
Siáght Meeh
Mt = 1
254
Flow rate at the design
N.S.W
ne
Transcribed Image Text:A supersonic diffuser a fixed geometry inlet is operating at sea level where the temperature 417K 2ら4 and pressure are K, and 1 kPA), respectively. The inlet and throat cross - sectional 0149 m2 areas are ( m² and m²), respectively. Determine: O.176 m? (a) The Mach number to which the inlet must be over expanded for starting. (b) The Mach number for which the inlet is designed. 417K x y G The mass- Srow-rate at When tue Too-OK hiet is dests overrenponnled fur Start Potalk Pa d- the mers - Siáght Meeh Mt = 1 254 Flow rate at the design N.S.W ne
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