Effect of Initial Grain Temperature on Combustion Response of Composite Solid Propellants in T-burner
Author:
Affiliation:
1. Defence Research and Development Laboratory, Defence Research and Development Organisation, Hyderabad, India
2. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, India
Funder
Defence Research and Development Organisation, Ministry of Defence, Govt. of India
Publisher
Informa UK Limited
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/00102202.2022.2121162
Reference19 articles.
1. REDUCED-ORDER MODELING AND DYNAMICS OF NONLINEAR ACOUSTIC WAVES IN A COMBUSTION CHAMBER
2. Pulse-Triggered Instability in Solid Rocket Motors
3. Pulsed instability in rocket motors - A comparison between predictions and experiments
4. Combustion instability of solid propellants
5. Examples of unsteady combustion in non-metallized propellants
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