| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000nam a2200000Ii 4500 |
| 001 |
in00004050849 |
| 005 |
20190307111342.0 |
| 006 |
m o d f |
| 007 |
cr ||||||||||| |
| 008 |
190102e201811 caua obt f000 0 eng d |
| 035 |
|
|
|a (OCoLC)on1080576806
|
| 040 |
|
|
|a GPO
|b eng
|e rda
|e pn
|c GPO
|d MvI
|
| 049 |
|
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|a WWW
|
| 074 |
|
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|a 0830-D (online)
|
| 086 |
0 |
|
|a NAS 1.15:2018-219788
|
| 100 |
1 |
|
|a Koning, Witold J. F.,
|e author.
|
| 245 |
1 |
0 |
|a Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /
|c Witold J. F. Koning [and three others].
|
| 264 |
|
1 |
|a Moffett Field, CA :
|b National Aeronautics and Space Administration, Ames Research Center,
|c November 2018.
|
| 300 |
|
|
|a 1 online resource (viii, 32 pages) :
|b color illustrations.
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
|
|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a NASA/TM ;
|v 2018-219788
|
| 500 |
|
|
|a "November 2018."
|
| 504 |
|
|
|a Includes bibliographical references (page 32).
|
| 588 |
|
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|a Description based on online resource, PDF version; title from title page (NASA, viewed Jan. 2, 2019).
|
| 650 |
|
7 |
|a Angle of attack.
|2 nasat
|
| 650 |
|
7 |
|a Directional stability.
|2 nasat
|
| 650 |
|
7 |
|a Rotary wing aircraft.
|2 nasat
|
| 650 |
|
7 |
|a Computational fluid dynamics.
|2 nasat
|
| 650 |
|
7 |
|a Wind tunnel tests.
|2 nasat
|
| 710 |
2 |
|
|a Ames Research Center,
|e issuing body.
|
| 830 |
|
0 |
|a NASA technical memorandum ;
|v 2018-219788.
|
| 856 |
4 |
0 |
|u https://purl.fdlp.gov/GPO/gpo114085
|t 0
|
| 999 |
f |
f |
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|i 2379625d-2df4-33f7-bd0e-4989b8bcad88
|t 0
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|d Available Online
|t 0
|e NAS 1.15:2018-219788
|h Superintendent of Documents classification
|
| 998 |
f |
f |
|a NAS 1.15:2018-219788
|t 0
|l Available Online
|