Explore topic-wise MCQs in Aircraft Design Questions and Answers.

This section includes 1 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design Questions and Answers knowledge and support exam preparation. Choose a topic below to get started.

1.

At exhaust of nozzle temperature is 200k and density of the flow is 1.01 kg/m3. If back pressure is 1 bar then, nozzle is ______________

A. nozzle can be under or over expanded
B. under expansion
C. over expanded
D. design condition
Answer» D. design condition
Discussion