Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors-Reference-Cited by-同舟云学术

Numerical Model to Analyze Transient Behavior and Instabilities on Hybrid Rocket Motors

Published:2015-03 Issue:2 Volume:31 Page:643-653
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Barato F.¹,Bellomo N.¹,Faenza M.¹,Lazzarin M.¹,Bettella A.²,Pavarin D.¹

Affiliation:

1. Department of Industrial Engineering, Center of Studies and Activities for Space, University of Padua, 35131 Padua, Italy

2. Technology for Propulsion and Innovation, S.r.l., 35137 Padua, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35282

Reference21 articles.

1. CulickF. E. C. “Unsteady Motions in Combustion Chambers for Propulsion Systems,” Research and Technology Organization AGARDograph AG-AVT-039, Neuilly-sur-Seine Cedex, France, Dec. 2006.

2. WooldridgeC.MarxmanG. A.KierR. “Investigation of Combustion Instability in Hybrid Rockets,” Final Rept. NASA CR-66812, 1969.

3. Acoustics, Vortex Shedding, and Low-Frequency Dynamics Interaction in an Unstable Hybrid Rocket

4. The Effects of Swirl Injector Design on Hybrid Flame-Holding Combustion Instability

5. Hybrid Propulsion Demonstration Program 250K Hybrid Motor

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities;AIAA SCITECH 2024 Forum;2024-01-04

2. Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket;Journal of Propulsion and Power;2022-10-07

3. Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor;Journal of Propulsion and Power;2022-09

4. Multiphysics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability;AIAA AVIATION 2022 Forum;2022-06-20

5. Regression rate modeling of HTPB/paraffin fuels in hybrid rocket motor;Aerospace Science and Technology;2022-02