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How to find throat area at the nozzle in single stage turbine? | GATE AE | Propulsion

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Disclaimer: The following content is just shared for educational purpose only and not originally created by WINGS of AERO Team. The credits always belong to Its respective publishers. Q : In a single-stage turbine designed on free vortex theory the following particulars are given : Mass flow through turbine – 18 kg/s; Inlet total head Read more about How to find throat area at the nozzle in single stage turbine? | GATE AE | Propulsion[…]

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1 Authorised medical examiner. 2 Alternate [alternative is meant] mission equipment. 3 Air Mobility Element (USAF). 4 Angle-measuring equipment. 5 Amplitude-modulation equivalent, or equipment. 6 Aircraft, multi-engine [L adds land, S sea]. 7 Aviation Maintenance Engineers Association [Fredericton, NB, Canada].  




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