Experimental Investigations of a Diffuser Start/Unstart Characteristics for Two Stream Supersonic Wind Tunnel
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-91017-8_139
Reference10 articles.
1. V.A. Amatucci, J.C. Dutton, A.L. Addy, Pressure recovery in a constant-area, two-stream supersonic diffuser. AIAA J. 20, 1308–1309 (1982)
2. R.J. Driscoll, L.F. Moon, Pressure recovery in chemical lasers. AIAA J. 15, 665–673 (1977)
3. J.C. Dutton, D. Mikkelsen, A.L. Addy, A theoretical and experimental investigation of the constant area, supersonic-supersonic ejector. AIAA J. 20, 1392–1400 (1982)
4. R.M. Kumaran, T. Sundararajan, D.R. Manohar, Performance evaluation of second-throat diffuser for high-altitude-test facility. J. Propuls. Power 26, 248–258 (2010)
5. D. Papamoschou, Diffuser performance of two-stream supersonic wind tunnels. AIAA J. 27, 1124–1127 (1988)
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