Course Hive
Search

Welcome

Sign in or create your account

Continue with Google
or
Similarity Parameters, Aerospace Engineering Lecture 20
Play lesson

Aerospace Engineering Lectures - Similarity Parameters, Aerospace Engineering Lecture 20

4.0 (1)
16 learners

What you'll learn

This course includes

  • 22.3 hours of video
  • Certificate of completion
  • Access on mobile and TV

Summary

Keywords

Full Transcript

The dynamic similarity parameters for wind tunnel testing are the Reynolds number and Mach number. The difficulty of getting these two numbers to match between the actual aircraft and the scaled model in the wind tunnel are pointed out. #aerospaceengineering #gateaerospaceengineering #aerodynamics #fluidmechanics

Course Hive

Continue this lesson in the app

Install CourseHive on Android or iOS to keep learning while you move.

Related Courses

FAQs

Course Hive
Download CourseHive
Keep learning anywhere