Periyapatna A. Ramakrishna
Professor
+91-44 2257 4018 (Work)
Publications - 59Publications - 59
Publications - 59Publications (60)
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ArticlesCombustion characteristics of aluminum–water gelled composite propellant2018 | American Institute of Aeronautics and Astronautics Inc.
ArticlesEnhancement of Aluminum Reactivity to Achieve High Burn Rate for an End Burning Rocket Motor2017 | Wiley-VCH Verlag
ArticlesExtinction of AP monopropellant by rapid depressurization: Computational and experimental studies2017 | Elsevier Inc.
ConferencesEffects of thermal properties on low pressure deflagration limit of AP2017 | Combustion Institute- ArticlesAttaining hypersonic flight with aluminum-based fuel-rich propellant2017 | American Institute of Aeronautics and Astronautics Inc.
- ConferencesEffect of ageing on mechanical properties of composite solid propellants2016 | American Institute of Aeronautics and Astronautics Inc, AIAA
- ArticlesBurning rate studies: Potassium-doped ammonium perchlorate with other burn-rate modifiers2016 | American Institute of Aeronautics and Astronautics Inc.
- ConferencesReducing residue in aluminized fuel-rich propellant for ramjets2016 | American Institute of Aeronautics and Astronautics Inc, AIAA
- ArticlesEffect of mechanical activation of high specific surface area aluminium with PTFE on composite solid propellant2016 | Elsevier Inc.
- Numerical Method to Estimate Thermal Conductivity of a Model Composite Propellant2016 | American Institute of Aeronautics and Astronautics
- ArticlesReducing Agglomeration of Ammonium Perchlorate Using Activated Charcoal2015 | Wiley-VCH Verlag
- ArticlesEnhancing composite solid propellant burning rates with potassium doped ammonium perchlorate-Part i2014 | American Institute of Aeronautics and Astronautics Inc.
- ConferencesEnhancing composite solid propellant burning rates with potassium doped ammonium perchlorate-part 22014 | American Institute of Aeronautics and Astronautics Inc.
- ArticlesMeasurement of regression rate in hybrid rocket using combustion chamber pressure2014 | Elsevier Ltd
- ArticlesEnhancement of hybrid fuel regression rate using a bluff body2014 | American Institute of Aeronautics and Astronautics Inc.
