Exam
Vibe
Home
Engineering
Aerospace Engineering
Biomedical Engineering
Chemical Engineering
Civil Engineering
Computer Science
Electrical Engineering
Electronics and Communication Engineering
Mechanical Engineering
Govt Exam
Banking Exams
Other Government
Police
Railway Exams
SSC
State PSC Exams
Teaching / Education Exams
UPSC Exams
Blog
Contact
๐
Home
โบ
Aerospace Engineering
โบ
Hypersonic Aerodynamics MCQ
โบ
Hypersonic boundary layer may transition to tur...
Hypersonic boundary layer may transition to turbulence due to:
A. Low Reynolds number
B. High Mach number and surface roughness
C. Low temperature
D. No-slip condition
Explanation:
Turbulence occurs at high Mach numbers and due to surface irregularities.
Tags:
Hypersonic Aerodynamics MCQ
,
Aerospace Engineering
ยซ Previous
Next ยป
More from Hypersonic Aerodynamics MCQ:
Hypersonic flow is generally defined as flow with Mach number greater than:
At hypersonic speeds, which phenomenon significantly affects aerodynamic heating?
Which type of shock wave is commonly formed in front of a blunt body at hypersonic speeds?
Hypersonic flow is dominated by:
Which parameter is critical in designing thermal protection for hypersonic vehicles?
The shock layer thickness decreases with:
Explore more in Aerospace Engineering:
Aerodynamics MCQs MCQs
Flight Mechanics MCQ MCQs
Aircraft Structures MCQs
Propulsion MCQ MCQs
Avionics MCQ MCQs
Aircraft Design MCQs
Spacecraft Engineering MCQ MCQs
Orbital Mechanics MCQ MCQs
Aerospace Materials MCQ MCQs
Flight Testing MCQ MCQs