Abstract
In the present study, experiments on liquid-fuel air-breathing pulse detonation engines (PDEs) are conducted using a low-vapor-pressure fuel: Jet A-1. Past studies have mostly focused on demonstrating the use of high-vapor-pressure fuels (e.g., heptane) or low-vapor-pressure fuels (e.g., JP8 and Jet A-1) with a predetermined air temperature (e.g., 398 K) or with some pretreatments on the liquid fuels (e.g., preheating of fuel). Based on previous notable studies [1–3], critical conditions for success or failure of liquid-fuel PDEs are mainly related to fuel types, inlet air temperatures, and spray droplet sizes. Essentially, these conditions determine the amount of pre-vaporized fuel prior to ignition. The present paper attempts to establish a criterion for detonation transition of two-phase Jet A-1/air mixtures.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Brophy, C.M., Netzer, D.W., Sinibaldi, J., Johnson, R.: High-speed Deflagration and Detonation: Fundamentals and Control Edited by G.D. Roy, S.M. Frolov, D.W. Netzer, amd A.A. Borisov. ELEX-KM Publishers, 2001. Moscow. pp. 207–222 (2001)
Tucker, K.C., King, P.I., Schauer, F.R.: J Propul. Power, 24(4): 788–796 (2008)
Frolov, S.M.: J Propul. Power. 22(6): 1162–1169 (2006)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2017 Springer International Publishing AG
About this paper
Cite this paper
Li, J., Juay, T.C., Li, L., Chang, P.H., Khoo, BC. (2017). Criterion for Detonation Transition in Liquid-Fuel Pulse Detonation Engines. In: Ben-Dor, G., Sadot, O., Igra, O. (eds) 30th International Symposium on Shock Waves 1. Springer, Cham. https://doi.org/10.1007/978-3-319-46213-4_69
Download citation
DOI: https://doi.org/10.1007/978-3-319-46213-4_69
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-46211-0
Online ISBN: 978-3-319-46213-4
eBook Packages: EngineeringEngineering (R0)