| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000cam a2200000Ia 4500 |
| 001 |
in00002192607 |
| 005 |
20211202204254.0 |
| 007 |
he bmb024bbca |
| 008 |
920219s1989 caua bbt f000 0 eng d |
| 019 |
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|a 24772918
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| 035 |
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|a (OCoLC)ocm25300351
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| 037 |
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|a N 90-13332
|b NASA
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| 040 |
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|a OKX
|c OKX
|d OCL
|d GPO
|d MvI
|d UtOrBLW
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| 049 |
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|a UMIC
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| 049 |
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|a WWW
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| 074 |
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|a 0830-D (MF)
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| 074 |
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|a 0830-D (online)
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| 086 |
0 |
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|a NAS 1.15:102196
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| 088 |
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|a A-89148
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| 100 |
1 |
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|a Browne, Lindsay E.
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| 245 |
1 |
0 |
|a Study of the integration of wind tunnel and computational methods for aerodynamic configurations /
|c Lindsay E. Browne and Dale L. Ashby.
|
| 264 |
|
1 |
|a Moffett Field, Calif. :
|b National Aeronautics and Space Administration, Ames Research Center ;
|c [1989]
|
| 264 |
|
2 |
|a [Springfield, Va.] :
|b [For sale by the National Technical Information Service],
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| 300 |
|
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|a vi, 66 pages :
|b illustrations
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| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a microform
|b h
|2 rdamedia
|
| 338 |
|
|
|a microfiche
|b he
|2 rdacarrier
|
| 490 |
1 |
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|a NASA technical memorandum ;
|v 102196
|
| 500 |
|
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|a "Performing organization report number: A-89148"--Technical rept. documentation p.
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| 500 |
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|a "October 1989."
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| 500 |
|
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|a Shipping list number: 90-0561-M.
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| 504 |
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|a Includes bibliographical references (page 43).
|
| 530 |
|
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|a Also available via Internet from the NASA Technical Report Server web site. Address as of 6/6/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004016%5F1990004016.pdf; current access available via PURL.
|
| 533 |
|
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|a Microfiche.
|b [Washington, D.C.? :
|c National Aeronautics and Space Administration,
|d 1990].
|e 1 microfiche : negative.
|
| 536 |
|
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|h 505-68-71
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| 500 |
|
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|a Microform.
|
| 650 |
|
0 |
|a Wind tunnel walls.
|
| 650 |
|
0 |
|a Aerodynamics
|x Mathematical models.
|
| 650 |
|
7 |
|a Aerodynamic configurations.
|2 nasat
|
| 650 |
|
7 |
|a Computational fluid dynamics.
|2 nasat
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| 650 |
|
7 |
|a Flow distribution.
|2 nasat
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| 650 |
|
7 |
|a Panel method (Fluid dynamics)
|2 nasat
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| 650 |
|
7 |
|a Wall flow.
|2 nasat
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| 650 |
|
7 |
|a Wind tunnel tests.
|2 nasat
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| 650 |
|
7 |
|a Wind tunnel walls.
|2 nasat
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| 700 |
1 |
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|a Ashby, Dale L.
|
| 710 |
2 |
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|a Ames Research Center.
|
| 830 |
|
0 |
|a NASA technical memorandum ;
|v 102196.
|
| 856 |
4 |
1 |
|u https://purl.fdlp.gov/GPO/LPS70437
|t 0
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| 952 |
f |
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|p normal
|a Texas A&M University
|b College Station
|c Sterling C. Evans Library
|d Evans: US Documents Microfiche (3rd floor)
|t 0
|e NAS 1.15:102196
|h Superintendent of Documents classification
|i microform -- microfiche
|m A14836112183
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|d Available Online
|t 0
|e NAS 1.15:102196
|h Superintendent of Documents classification
|
| 998 |
f |
f |
|a NAS 1.15:102196
|t 0
|l Available Online
|
| 998 |
f |
f |
|a NAS 1.15:102196
|t 0
|l Evans: US Documents Microfiche (3rd floor)
|