An ideal turbofan operates at 11,000m with a free-stream Mach number of 0.85. Considering the following...

60.1K

Verified Solution

Question

Mechanical Engineering

An ideal turbofan operates at 11,000m with a free-stream Machnumber of 0.85. Considering the following design inputs:

Bypass ratio:?= 8

Fan pressure ratio:?F= 1.6

Compressor pressure ratio:?c= 25

Fuel heating energy:hPR= 43,500kJ/kg

Total temperature downstream of the combustor:Tt4= 1420K

a)Calculate all the points and plot the thermodynamic cycle ofthe core flow on a T-sdiagram.

b)Calculate specific thrust, specific fuel consumption, thermalefficiency, propulsive efficiency and overall efficiency.

c)Compare the performance parameters in part b)with those of anideal turbojet with the same ?c, Tt4 and hPR.

Answer & Explanation Solved by verified expert
3.6 Ratings (617 Votes)
    See Answer
Get Answers to Unlimited Questions

Join us to gain access to millions of questions and expert answers. Enjoy exclusive benefits tailored just for you!

Membership Benefits:
  • Unlimited Question Access with detailed Answers
  • Zin AI - 3 Million Words
  • 10 Dall-E 3 Images
  • 20 Plot Generations
  • Conversation with Dialogue Memory
  • No Ads, Ever!
  • Access to Our Best AI Platform: Flex AI - Your personal assistant for all your inquiries!
Become a Member

Other questions asked by students