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00000cam a2200000Ka 4500 |
| 001 |
in00002780124 |
| 005 |
20150922143046.0 |
| 006 |
m fo d |
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cr unu|||||||| |
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121114s2012 txu obm 000 0 eng d |
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|a (OCoLC)ocn817968533
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| 035 |
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|a (OCoLC)817968533
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| 035 |
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|a (TxCM)http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524
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| 040 |
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|a TXA
|c TXA
|d UtOrBLW
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| 049 |
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|a TXAM
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|a 2012
|a Thesis
|a 1969.1/ETD-TAMU-2012-08-11524
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|a Taylor, David Christopher.
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|a The characterization and feasibility of a low-duty-cycle diaphragmless shock tube /
|c by David Christopher Taylor.
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|a [College Station, Tex.] :
|b [Texas A&M University],
|c [2012]
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|a 1 online resource.
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 500 |
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|a "Major Subject: Aerospace Engineering"
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|a Description from author supplied metadata (automated record created 2012-10-22 13:24:58).
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| 502 |
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|b Master of Science
|c Texas A&M University
|d 2012
|o http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524
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|a Includes bibliographical references.
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| 516 |
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|a Text (Thesis)
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|a The feasibility and characterization of a novel diaphragmless shock tube was examined at the National Aerothermochemistry Laboratory at Texas A&M University. The goal was to design a facility that reliably produces shock waves through air in a repeatable manner sufficient for statistical analysis. The device is modular, automated, and compact. The proposed diaphragmless shock tube uses a shock wave generating mechanism that consists of a rotating door and locking cam-shaft system. The facility produced the desired driver gas pressures repeatedly to within 0.31% at low-duty-cycle of 6 seconds. The driven gas pressure profiles within the test-section suggest that shock waves may be forming within test section for a driver gas pressure of 200 psig and above, which corresponds to shock wave Mach numbers of 1.7 to 2.0. The measured wave speeds were within 3.1% of that predicted by ideal shock tube theory; however, the induced driven gas pressures within the constant pressure region were approximately half that expedited from ideal shock tube theory.
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|a Electronic resource.
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|a Major Aerospace Engineering.
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|a Shock Tube
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| 653 |
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|a Aerospace Engineering
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| 653 |
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|a Facility Development
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| 700 |
1 |
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|a Bowersox, Rodney D. W.,
|e thesis advisor.
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| 856 |
4 |
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|u http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11524
|z Link to OAK Trust copy
|t 0
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| 994 |
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|a C0
|b TXA
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| 948 |
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|a cataloged
|b h
|c 2012/11/14
|d o
|e blrosas
|f 1:41:58 pm
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| 999 |
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|a MARS
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| 999 |
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f |
|s 52553abb-746c-3503-a161-1f51c13cc36a
|i 57930b4c-f3b5-313c-8c26-1b57d088bef2
|t 0
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| 952 |
f |
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|a Texas A&M University
|b College Station
|c Electronic Resources
|d Available Online
|t 0
|e 2012 Thesis 1969.1/ETD-TAMU-2012-08-11524
|h Other scheme
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| 998 |
f |
f |
|a 2012 Thesis 1969.1/ETD-TAMU-2012-08-11524
|t 0
|l Available Online
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