Modification of Flow Characteristics on the Blowing Surface by Inserting a Diaphragm
Author:
Affiliation:
1. Department of Aerospace Engineering, Konkuk University, Seoul 143-701, Republic of Korea
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.B35361
Reference15 articles.
1. Effect of a Diaphragm on Performance and Fuel Regression of a Laboratory Scale Hybrid Rocket Motor Using Nitrous Oxide and Paraffin
2. LazzarinM.PavarinD.ManenteM. “Advanced Fluid Dynamic Codes for Propellant Behavior, Injection and Combustion Simulation in Hybrid Rockets,” Ph.D. Thesis, Univ. of Padova, Padova, Italy, 2012.
3. Effect of Protrusion in the Enhancement of Regression Rate in Hybrid Rocket
4. Effect of Diaphragms on Regression Rate in Hybrid Rocket Motors
5. Role of Injection in Hybrid Rockets Regression Rate Behaviour
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