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Design and Characterization of a Hypervelocity Expansion Tube Facility

Dufrene, A. and Sharma, M. and Austin, J. M. (2007) Design and Characterization of a Hypervelocity Expansion Tube Facility. Journal of Propulsion and Power, 23 (6). pp. 1185-1193. ISSN 0748-4658.

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We report on the design and characterization of a 152-mm-diam expansion tube capable of accessing a range of high-enthalpy test conditions with Mach numbers up to 7.1. Expansion tubes have the potential to offer a wide range of test flow conditions as gas acceleration is achieved through interaction with an unsteady expansion wave rather than expansion through a fixed-area-ratio nozzle. However, the range of test flow conditions is limited in practice by a number of considerations such as a short test time and large-amplitude flow disturbances. We present a generalized design strategy for small-scale expansion tubes. As a starting point, ideal gasdynamic calculations for optimal facility design to maximize test time at a given Mach number test condition are presented, together with a correction for the expansion-head reflection through a nonsimple region. A compilation of practical limitations that have been identified for expansion tube facilities, such as diaphragm rupture and flow-disturbance minimization, is then used to map out a functional design parameter space. Experimentally, a range of test conditions are verified through pitot pressure measurements and analysis of schlieren images of flow over simple geometries. To date, there has been good agreement between theoretical and experimental results.

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Additional Information:© 2007 by the University of Illinois at Urbana–Champaign. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Presented as Paper 1327 at the 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 8–11 January 2007; received 8 February 2007; revision received 14 June 2007; accepted for publication 16 June 2007. This research was funded in part through a Multi-University Research Initiative (MURI) granted by the U.S. Air Force Office of Scientific Research (AFOSR), with John Schmisseur as Technical Monitor. Special thanks to Matthew D. Parker for test-section design and construction and data acquisition system installation, to Matthew McGilvray for the design of the transducer mounts, and to Richard Morgan for helpful discussions.
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Air Force Office of Scientific Research (AFOSR) Multidisciplinary University Research Initiative (MURI)UNSPECIFIED
Issue or Number:6
Record Number:CaltechAUTHORS:20140924-085848815
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Official Citation:A. Dufrene, M. Sharma, and J. M. Austin. "Design and Characterization of a Hypervelocity Expansion Tube Facility", Journal of Propulsion and Power, Vol. 23, No. 6 (2007), pp. 1185-1193. doi: 10.2514/1.30349
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:49976
Deposited By: Tony Diaz
Deposited On:29 Sep 2014 22:21
Last Modified:03 Oct 2019 07:18

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