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991020s1996 dcu b f100 0 eng d |
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|a (OCoLC)ocm42671384
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|a 19960054470
|b NASA
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|a GPO
|b eng
|c GPO
|d SYB
|d OCLCF
|d OCLCO
|d OCLCQ
|d OCLCO
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|d GPO
|d MvI
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|a COD9
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|a 0830-D (MF)
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|a NAS 1.15:110484
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|a NAS 1.15:110484
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| 111 |
2 |
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|a Euromech Colloquium
|n (349th :
|d 1996 :
|c Göttingen, Germany)
|
| 245 |
1 |
0 |
|a Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
|h [microform] :
|b EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 /
|c John W. Edwards.
|
| 246 |
3 |
0 |
|a EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996.
|
| 264 |
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1 |
|a [Washington, DC] :
|b [National Aeronautics and Space Administration] ;
|a [Springfield, Va.] :
|b [National Technical Information Service, distributor],
|c [1996]
|
| 300 |
|
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|a 1 volume.
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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 microform
|b h
|2 rdamedia.
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| 338 |
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|a microfiche
|b he
|2 rdacarrier.
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| 490 |
1 |
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|a NASA-TM ;
|v 110484.
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| 500 |
|
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|a Shipping list number: 97-0681-M.
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| 533 |
|
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|a Microfiche.
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,
|d 1997].
|e 1 microfiche.
|
| 650 |
|
7 |
|a Separated flow.
|2 nasat.
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| 650 |
|
7 |
|a Transonic flow.
|2 nasat.
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| 650 |
|
7 |
|a Transonic flutter.
|2 nasat.
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| 650 |
|
7 |
|a Transonic speed.
|2 nasat.
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| 650 |
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7 |
|a Unsteady flow.
|2 nasat.
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| 650 |
|
7 |
|a Viscous flow.
|2 nasat.
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| 650 |
|
7 |
|a Computational fluid dynamics.
|2 nasat.
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| 650 |
|
7 |
|a Coupling.
|2 nasat.
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| 650 |
|
7 |
|a Airfoils.
|2 nasat.
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| 650 |
|
7 |
|a Mach number.
|2 nasat.
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| 650 |
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7 |
|a Boundary layer separation.
|2 nasat.
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| 650 |
|
7 |
|a Airfoil oscillations.
|2 nasat.
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| 700 |
1 |
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|a Edwards, John W.
|0 http://id.loc.gov/authorities/names/n94033842.
|
| 710 |
1 |
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|a United States.
|b National Aeronautics and Space Administration.
|0 http://id.loc.gov/authorities/names/n78087581
|1 http://isni.org/isni/0000000449071619.
|
| 776 |
0 |
8 |
|i Online version:
|a Edwards, John W.
|t Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
|w (OCoLC)990066147.
|
| 830 |
|
0 |
|a NASA technical memorandum ;
|v 110484.
|0 http://id.loc.gov/authorities/names/n83707893.
|
| 907 |
|
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|a .b30888736
|b 04-05-22
|c 11-12-99
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| 998 |
|
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|a gov
|b 12-15-99
|c -
|d m
|e -
|f eng
|g dcu
|h 0
|i 2
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| 907 |
|
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|a .b30888736
|b 05-08-19
|c 11-12-99
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| 944 |
|
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|a MARS - RDA ENRICHED
|
| 999 |
f |
f |
|i 7e4404b2-bc1e-57eb-9fcc-9fc1d85d5b6a
|s 9cd1926e-2008-5429-ba39-924c61fe0072
|
| 952 |
f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Norlin
|d Norlin Library - Government Information - Microform
|e NAS 1.15:110484
|h Superintendent of Documents classification
|i document
|n 1
|
