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Değirmenci et al., 2016 - Google Patents

Thermo-mechanical analysis of double base propellant combustion in a barrel

Değirmenci et al., 2016

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Document ID
2341246073020474802
Author
Değirmenci E
Evci C
Işık H
Macar M
Yılmaz N
Dirikolu M
Çelik V
Publication year
Publication venue
Applied Thermal Engineering

External Links

Snippet

Accurate determination of burning characteristics of the propellant and thermo-mechanical loads acting on the barrel supports better gun design and its tactical use. As the frequency of successive shots changes, burning rate of the gun propellant also changes and …
Continue reading at www.academia.edu (PDF) (other versions)

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/96—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by specially adapted arrangements for testing or measuring

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