Study of Detonation Interactions Inside a Two-Dimensional Ejector Using Detonation Transmission Tubing
Author:
Affiliation:
1. University of Manchester, Manchester, England M60 1QD, United Kingdom
2. Indian Institute of Science, Bangalore 560 012, India
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/10.2514/1.44338
Reference20 articles.
1. Structural characteristics of detonation expansion from a small channel to a larger one
2. Thrust Chamber Dynamics and Propulsive Performance of Single-Tube Pulse Detonation Engines
3. Interactions Between Shock and Acoustic Waves in a Supersonic Inlet Diffuser
4. Diffraction and re-initiation of detonations behind a backward-facing step
5. Parametric Investigation of Thrust Augmentation by Ejectors on a Pulsed Detonation Tube
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