Experimental Investigations on DDT Enhancements by Schelkin Spirals in a PDE

Author:

New T.1,Panicker Philip2,Lu Frank2,Tsai H.1

Affiliation:

1. National University of Singapore

2. University of Texas at Arlington

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Direct Experimental Impulse Measurements for Detonations and Deflagrations

2. 3Lee S-Y, Watts J., Saretto S., Pal S., Conrad C., Woodward R. and Santoro R. "Deflagration to detonation transition processes by turbulence-generating obstacles in pulse detonation engines," Journal of Propulsion and Power,Vol.20,No.6,pp.1026-1036,2004.

3. 4Lu F.K., Meyers J.M., and Wilson D.R. "Experimental study of a pulse detonation rocket with Shchelkin spiral,"AIAAPaper2003-6974,2003.

4. 5Li, C., and Kailasanath, K. "A numerical study of reactive flows in pulsed detonation engines," AIAA Paper 2001-3933,2001.

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