Pregled bibliografske jedinice broj: 298120
Numerical Modelling of Effect of Heating Rate on Results of Dynamic Mechanical Analysis of a Rocket Propellant
Numerical Modelling of Effect of Heating Rate on Results of Dynamic Mechanical Analysis of a Rocket Propellant // 10th Seminar on New Trends in Research of Energetic Materials : proceedings / Ottis, Jan ; Krupka, Miroslav (ur.).
Pardubice: University of Pardubice, 2007. str. 904-916 (poster, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
CROSBI ID: 298120 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Numerical Modelling of Effect of Heating Rate on Results of Dynamic Mechanical Analysis of a Rocket Propellant
Autori
Sućeska, Muhamed ; Liu, Zhi-Yue ; Matečić Mušanić, Sanja
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
10th Seminar on New Trends in Research of Energetic Materials : proceedings
/ Ottis, Jan ; Krupka, Miroslav - Pardubice : University of Pardubice, 2007, 904-916
ISBN
978-80-7194-949-7
Skup
Seminar on New Trends in Research of Energetic Materials (10 ; 2007)
Mjesto i datum
Pardubice, Češka Republika, 25.04.2007. - 27.04.2007
Vrsta sudjelovanja
Poster
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
thermal methods; dynamic mechanical analysis; heat conduction equation; double base rocket propellants; thermal lag; thermal gradient
Sažetak
Thermal methods play important role in the analysis of explosives. The most frequently these methods are used for the characterisations and determination of the thermal, thermomechanical, and thermokinetic properties of explosives. Due to dynamic nature of processes taking place during the experiment (chemical reaction and physical processes, heat flow, gas flow, etc.) results obtained by thermal methods may considerably depend on the conditions used during the experiment. Therefore, whenever results of thermal analysis are reported, the experimental conditions used should be stated. In this paper we have studied the heat transfer from the furnace to the sample, and through the sample, during dynamic mechanical analysis (DMA) measurements. Numerical modelling of the heat transfer was done using an own computer program based on the reactive heat conduction equation, solved numerically applying the finite difference methods. The calculated values of thermal lag between the furnace and sample were compared with values determined experimentally on samples of double-base rocket propellant at different heating rates. Also, the temperature distribution within the sample as a function of the heating rate was analysed using the same numerical model. It was shown that even at slow heating rates there is significant thermal lag between the furnace and sample, as well as significant thermal gradient within the sample.
Izvorni jezik
Engleski
Znanstvena područja
Kemija, Kemijsko inženjerstvo
POVEZANOST RADA
Projekti:
192-1252971-1982 - Istraživanje procesa starenja i predikcija životnog vijeka materijala (Sućeska, Muhamed, MZOS ) ( CroRIS)
Ustanove:
Brodarski institut d.o.o.