PLIF imaging and thermometry of NO/N2 shock layer flows in an expansion tube
Author:
Affiliation:
1. Australian National Univ., Canberra, Australia
2. Stanford Univ., CA
3. Queensland, Univ., Saint Lucia, Australia
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-537
Reference25 articles.
1. 12 for Accelerating Projectiles to UltrahighVelocities," AIAA Journal, Vol.26, 1988,pp195-203.
2. New expansion tube facility for the investigation of hypersonic reactive flow
3. Palmer, J. L., Houwing, A. F. P., Thurber, M. C., Wehe, S. D. and Hanson, R. K. "PLIF Imaging of Transient Shock Phenomena in Hypersonic Flows", AIAA Paper No. 94-2642,1994.6.Houwing,A.F.P.,Palmer,J.L.,Boyce,R. R., Thurber, M. C., Wehe, S. D. and Hanson, R. K. "PLIF thermometry in a high temperature shock layer flow on a cylinder in a supersonicjet",AIAA Paper No.95-0515, 1995.
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