A supersonic diffuser a fixed geometry inlet is operating at sea level where the temperature417K2ら4and pressure are K, and 1 kPA), respectively. The inlet and throat cross - sectional0149 m2areas 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 yG The mass- Srow-rate at When tue Too-OKhiet is dests overrenponnled fur Start Potalk Pad- the mers -Siáght MeehMt = 1254Flow rate at the designN.S.Wne

T= 417 K P = 254 kPa A= 0.176 m2 A*=0.149 m2 k= 1.4 (for thermally perfect gas) To find- a) Mach…

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

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

Section: Chapter Questions

Problem 1P

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