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| LEADER |
00000ctm a22000005a 4500 |
| 001 |
in00001514913 |
| 005 |
20220103134724.0 |
| 007 |
cr unu a |
| 008 |
991026s1998 xx a b 000 0 eng d |
| 035 |
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|9 AJL0387AM
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| 035 |
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|a (OCoLC)42706176
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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
|a TXAR
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| 099 |
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|a 1998
|a Thesis
|a J63
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| 100 |
1 |
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|a Johansen, Espen S.
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| 245 |
1 |
0 |
|a Steady and unsteady calibration of multi-hole probes /
|c by Espen S. Johansen.
|
| 264 |
|
1 |
|a [Place of publication not identified] :
|b [publisher not identified] ;
|c 1998.
|
| 300 |
|
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|a xv, 71 leaves :
|b illustrations ;
|c 28 cm.
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a computer
|b c
|2 rdamedia
|
| 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".
|
| 500 |
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|a Vita.
|
| 502 |
|
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|b M.S.
|c Texas A&M University
|d 1998.
|
| 504 |
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|a Includes bibliographical references (leaves 65-67).
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| 520 |
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|a -based, fast-response, multi-sensor pressure probes of
|
| 520 |
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|a accurate predictions of the velocity magnitude and
|
| 520 |
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|a algorithm is able to reduce data from any 5- or 7-hole
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| 520 |
|
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|a also discussed. A new type of pressure sensor has been
|
| 520 |
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|a and experimental approaches are employed to develop
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| 520 |
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|a and viscosity. The algorithm utilizes a local least-
|
| 520 |
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|a applications in unsteady and turbulent flow gelds is
|
| 520 |
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|a been calibrated at NASA Langley Flow Modeling and
|
| 520 |
|
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|a calibration data from miniature non-nulling multi-hole
|
| 520 |
|
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|a calibration techniques suitable for highly unsteady
|
| 520 |
|
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|a characteristic size of only 250 gm. These pressure
|
| 520 |
|
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|a Control Branch for the entire subsonic regime. Each of
|
| 520 |
|
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|a degrees and maximum errors in velocity prediction less
|
| 520 |
|
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|a developed with silicon-nitride diaphragm and a
|
| 520 |
|
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|a development of Micro Electro Mechanical Systems (MEMS)
|
| 520 |
|
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|a direction, total and static pressure, Mach and
|
| 520 |
|
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|a Excellent prediction capabilities are demonstrated
|
| 520 |
|
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|a flow environments with strong spatial gradients.
|
| 520 |
|
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|a frequency response up to 100 kl-lz. Both computational
|
| 520 |
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|a miniature size for velocity and pressure measurement
|
| 520 |
|
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|a obtaining a probe bandwidth and a theoretical
|
| 520 |
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|a probe in a subsonic flow field and generate very
|
| 520 |
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|a probes in compressible, subsonic flow gelds. The
|
| 520 |
|
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|a reduction algorithm for multi-hole pressure probes.
|
| 520 |
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|a Reynolds member and fluid properties like the density
|
| 520 |
|
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|a sensors are small enough to be mounted close to the
|
| 520 |
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|a squares modeling technique and has been
|
| 520 |
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|a surface of a miniature hemispherical-tip probe,
|
| 520 |
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|a tested on 4 novel miniature 7-hole probes that have
|
| 520 |
|
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|a than 1%, both with 99 percent confidence. The
|
| 520 |
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|a The algorithm has been developed for the reduction of
|
| 520 |
|
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|a the probes had a conical tip with diameter of 0.065''.
|
| 520 |
|
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|a This thesis presents the development of a data crographics.
|
| 520 |
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|a with maximum errors in angle prediction less than 0.6
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| 530 |
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|a Also available online.
|
| 650 |
|
4 |
|a Major aerospace engineering.
|
| 856 |
4 |
1 |
|u https://hdl.handle.net/1969.1/ETD-TAMU-1998-THESIS-J63
|z Link to OAKTrust copy
|t 0
|
| 948 |
|
|
|a c:en
|
| 999 |
|
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|a MARS
|
| 999 |
f |
f |
|s ffef50e1-baa1-3d47-b56f-1438ab5116ce
|i 94da11cd-28c7-375d-9c29-202179cccc7c
|t 0
|
| 952 |
f |
f |
|p noncirc
|a Texas A&M University
|b College Station
|c Cushing Memorial Library & Archives
|s cush tdrm
|d Cushing: Theses & Dissertations Microforms (Does not check out)
|t 0
|e 1998 Thesis J63
|h Other scheme
|i computer -- online resource
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|s www_evans
|d Available Online
|t 0
|e 1998 Thesis J63
|h Other scheme
|
| 998 |
f |
f |
|a 1998 Thesis J63
|t 0
|l Available Online
|
| 998 |
f |
f |
|a 1998 Thesis J63
|t 0
|l Cushing: Theses & Dissertations Microforms (Does not check out)
|