Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

Title
Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor
Authors
Keywords
-
Journal
JOURNAL OF PROPULSION AND POWER
Volume 32, Issue 3, Pages 560-573
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2016-04-19
DOI
10.2514/1.b35768

Ask authors/readers for more resources

Discover Peeref hubs

Discuss science. Find collaborators. Network.

Join a conversation

Create your own webinar

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

Create Now