Quick Links
Take a Practice Exam
Contribute to the Site
Browse the Exams
About this Site
Privacy Policy
Terms & Conditions
Site Map
New User
Log In
Examine My Cookies
Contact WebMaster
Exams4Pilots Forum
Forum Home
- Latest News
- Testimonials
- Tips & Tricks
- Stuck Mike
- Bug Reports
- Feature Request
SiteMap
You are here:
home
->
amp
->
B02
->B.8.1.8.2.A.1
8182
The pressure of supersonic air as it flows through a divergent nozzle
A) decreases.
B) is inversely proportional to the temperature.
C) increases.
This site was made possible by:
Validate me