Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions

Title
Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions
Authors
Keywords
-
Journal
EXPERIMENTS IN FLUIDS
Volume 63, Issue 12, Pages -
Publisher
Springer Science and Business Media LLC
Online
2022-12-17
DOI
10.1007/s00348-022-03543-1

Ask authors/readers for more resources

Find Funding. Review Successful Grants.

Explore over 25,000 new funding opportunities and over 6,000,000 successful grants.

Explore

Create your own webinar

Interested in hosting your own webinar? Check the schedule and propose your idea to the Peeref Content Team.

Create Now