Ignition delay of 3-carene: single pulse shock tube study


Autoria(s): Sharath, N; Reddy, KPJ; Barhai, PK; Arunan, E
Data(s)

2015

Resumo

Ignition delay experiments of 3-carene, a biofuel, have been carried out in a single-pulse shock tube for three equivalence ratios, 0.5, 1 and 2. The temperature was varied from 1140 to 1606 K. In the above-mentioned conditions, ignition delay was found to vary from 1.180 ms to 144 mu s. The ignition delay values of 3-carene were found to be lower than those of JP-10, a kerosene-based fuel being considered for hypersonic applications.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/51919/1/Cur_Sci_108-11_2083_2015.pdf

Sharath, N and Reddy, KPJ and Barhai, PK and Arunan, E (2015) Ignition delay of 3-carene: single pulse shock tube study. In: CURRENT SCIENCE, 108 (11). pp. 2083-2087.

Publicador

INDIAN ACAD SCIENCES

Relação

http://www.currentscience.ac.in/Volumes/108/11/2083.pdf

http://eprints.iisc.ernet.in/51919/

Palavras-Chave #Inorganic & Physical Chemistry #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed