No Access
Aerothermodynamic simulation model for new hypersonic propulsion: Rocket Ignited Supersonic Combustion Ram Jet
AIAA 2016-5323
Session: Reusable Launch Vehicles and Technology
Published Online:9 Sep 2016https://doi.org/10.2514/6.2016-5323
- Cited by
-
What's Popular
Crossmark
Information
Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Topics
