BIPOLAR COMBUSTION RESPONSE MODEL FOR HYBRID ROCKET INTERNAL BALLISTIC SIMULATION (AIAA 2016-4565)
Joint propulsion conference
2016-01-01
11 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Hybrid Rocket Engine Transient Internal Ballistic Simulation (AIAA 2015-3834)
British Library Conference Proceedings | 2015
|Modeling Spray Combustion of Jet-A in a Constant-Volume Combustion Chamber (AIAA 2018-4565)
British Library Conference Proceedings | 2018
|DataCite | 1933