High Mach Number Scramjet Test Flows in the X3 Expansion Tube
作者： D. E. Gildfind , J. Sancho , R. G. Morgan
DOI: 10.1007/978-3-319-16835-7_58
关键词:
摘要: The University of Queensland (UQ) has two free-piston driven expansion tube facilities; X2 a total length 23 m and was originally commissioned in 1995 [1]; X3 is much longer at 62 m, 2001 [2].
uq.edu.au
springer.com
harvard.edu
core.ac.uk参考文章(8)
David E. Gildfind, Development of high total pressure scramjet flow conditions using the X2 expansion tube ,(2012)
R. J. Gollan, P. A. Jacobs, The Eilmer3 Code: user guide and example book The University of Queensland. pp. 1- 375 ,(2013)
S. Z. Pinckney, A short static-pressure probe design for supersonic flow STIN. ,vol. 75, pp. 27305- ,(1975)
R.G. Morgan, A two-stage free-piston driver Shock Waves. ,vol. 9, pp. 239- 248 ,(1999) , 10.1007/S001930050161
David Gildfind, Richard Morgan, Mathew McGilvray, Peter Jacobs, Simulation of High Mach Number Scramjet Flow Conditions using the X2 Expansion Tube 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. ,(2012) , 10.2514/6.2012-5954
Matthew McGilvray, Rainer Kirchhartz, Thomas Jazra, Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities AIAA Journal. ,vol. 48, pp. 1647- 1651 ,(2010) , 10.2514/1.J050025
Richard Morgan, Free piston-Driven expansion tubes Handbook of Shock Waves. pp. 603- 622 ,(2001) , 10.1016/B978-012086430-0/50014-2
RICHARD MORGAN, Chapter 4.3 - Shock Tubes and Tunnels: Facilities, Instrumentation, and Techniques pp. 603- 622 ,(2001) , 10.1016/B978-012086430-0/50014-2