Access provided by Rice University


John J. Bertin, Russell M. Cummings: Fifty years of hypersonics: where we've been, where we're going. Department of Aeronautics, Progress in Aerospace Sciences 39 (2003) 511-53.
CrossRef
Bertin JJ and Cummings RM: Critical hypersonic aerothermodynamic phenomena. Annu. Rev. Fluid Mech. 2006. 38:129-157.
CrossRef
Herbert Olivier, Zonglin Jiang, Hongyu Ru and Frank K. Lu: Detonation-driven shock tubes and tunnels, Advanced Hypersonic Test Facilities, published by AIAA, 135-203.
Holden MS: Design, development and calibration of the LENS facility, AFOSR-TR. 1994, 94-0161.
Holden MS, Wadhams TP, Candler GV: A review of experimental studies in the LENS shock tunnel and expansion tunnel to examine real-gas effects in hypervelocity flows, AIAA Paper 2004-0916, 42th AIAA Aerospace Sciences Meeting & Exhibit Reno, NV: January 5-8, 2004.
Holden MS, Chadwick KM, Kolly JM: Hypersonic studies in the LENS facilities, AIAA 95-6040, 6th International Aerospace Planes and Hypersonic Technologies Conferences, Chattanooga, Tennessee, April 3-7, 1995.
Stalker RJ: A study of the free-piston shock tunnel, AIAA J 5: 2160-2165, 1967.
Stalker RT and Morrson WRD.: New generation of free piston shock tunnel facilities, Proceeding of 17th International Symposium on Shock Tube and Waves, Bethem, 1989.
Hornung HG: The piston motion in a free-piston driver for shock tubes and tunnels. GALCIT Rep. FM88-1, 1988.
Itoh K, Ueda S et al.: Improvement of a free piston driver for a high-enthalpy shock tunnel, Shock Waves (1998) 8: 215-233
CrossRef
Itoh K, Ueda S, Tanno H, Komuro T, Sato K: Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel, Shock Waves (2002) 12: 93-98.
CrossRef
Bird GA: A note on combustion driven tubes, Royal Aircraft Establishment, AGARD Rep. P. 146, May 1957.
Yu HR, Esser B, Lenartz M, Gronig H: Gaseous detonation driver for a shock tunnel, Shock Waves, 1992, Vol. 2, 245-254.
CrossRef
Zhao W, Jiang ZL, Saito T., Lin JM, Yu HR and Takayama K: Performance of a detonation driven shock tunnel, Shock waves, (2005) Volume 14, Numbers 1-2, 53 - 59.
CrossRef
Habermann M, Olivier H and Grong H: Operation of a high performance detonation driver in upstream propagation mode for a hypersonic shock tunnel, Proceedings of the 22nd International Symposium on Shock Waves, Vol. 1, 1999, pp. 447-452.
Bakos RJ, Erdos JI: Options for enhancement of the performance of shock-expansion tubes and tunnels. AIAA 95-0799, 1995.
G. J. Wilson, M. A. Sussman, D. W. Bogdanoff: A study of combustion and detonation drivers for high enthalpy expansion tubes and shock tubes, NASA CDTP-20000. 1995.
Zonglin. Jiang, Wei Zhao, C. Wang: Forward-running detonation drivers for high-enthalpy shock tunnels, AIAA Journal, 40(10), 2002.