MCQOPTIONS
Bookmark
Saved Bookmarks
→
Aircraft Design
→
Longitudinal Static Stability Control 1 in Aircraft Design
→
Only convergent section will be used for supersoni..
1.
Only convergent section will be used for supersonic speeds.
A.
True
B.
False
Answer» B. False
Show Answer
Discussion
No Comment Found
Post Comment
Related MCQs
At exhaust of nozzle temperature is 200k and density of the flow is 1.01 kg/m<sup>3</sup>. If back pressure is 1 bar then, nozzle is ______________
____________ is the most common type of boundary layer diverter used for supersonic applications.
If area ratio is 1.110 then, at which mach number flow is flowing?
Our designed Mach number is 0.8. Find the required area ratio for the design. Assume isentropic relation is valid.
Consider a flow with 0.5M. Now, as area decreases, velocity of the flow inside convergent section _____________
Only convergent section will be used for supersonic speeds.
Performance of engine can be controlled by nozzle.
What is the function of a typical nozzle?
Reply to Comment
×
Name
*
Email
*
Comment
*
Submit Reply