A convergent-divergent nozzle expands air at 689 kPa and 427 °C to 100 kPa. The throat area of the nozzle is 650 and R

Business, Finance, Economics, Accounting, Operations Management, Computer Science, Electrical Engineering, Mechanical Engineering, Civil Engineering, Chemical Engineering, Algebra, Precalculus, Statistics and Probabilty, Advanced Math, Physics, Chemistry, Biology, Nursing, Psychology, Certifications, Tests, Prep, and more.
Post Reply
answerhappygod
Site Admin
Posts: 899603
Joined: Mon Aug 02, 2021 8:13 am

A convergent-divergent nozzle expands air at 689 kPa and 427 °C to 100 kPa. The throat area of the nozzle is 650 and R

Post by answerhappygod »

A convergent-divergent nozzle expands air at 689 kPa and 427 °C
to 100 kPa. The throat area of the nozzle is 650 and R for air is 287J/kg.K.
Assume gamma to be 1.4 and calculate the mass of air flow through
the nozzle in kilogram. The inlet velocity is negligible and
is 1.005
KJ/kg.K
Join a community of subject matter experts. Register for FREE to view solutions, replies, and use search function. Request answer by replying!
Top
Post Reply

Return to “Archived Questions & Answers”