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|a (OCoLC)ocn761308948
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|a OCLCE
|b eng
|e rda
|e pn
|c OCLCE
|d OCLCQ
|d OCLCF
|d OCLCQ
|d OCLCO
|d OCLCQ
|d GPO
|d MERUC
|d GPO
|d MvI
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|a pcc
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|a GDWR
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|a 0830-H-15 (online)
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0 |
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|a NAS 1.60:2565
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100 |
1 |
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|a Jenkins, Renaldo V.,
|e author.
|0 http://id.loc.gov/authorities/names/n84119130
|
245 |
1 |
0 |
|a R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /
|c Renaldo V. Jenkins.
|
264 |
|
1 |
|a Washington, D.C. :
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c May 1986.
|
300 |
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|a 1 online resource (111 pages) :
|b illustrations.
|
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.
|
490 |
1 |
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|a NASA/TP ;
|v 2565
|
500 |
|
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|a Prepared at Langley Research Center.
|
500 |
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|a "May 1986."
|
504 |
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|a Includes bibliographical references (pages 9-10)
|
513 |
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|a Technical paper.
|
588 |
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|a Description based on online resource, PDF version; title from title page (NASA, viewed July 16, 2018)
|
536 |
|
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|a Langley Research Center
|d 505-61-01-02
|d L-16066.
|
650 |
|
0 |
|a Aerofoils
|x Testing
|v Statistics.
|
650 |
|
0 |
|a Reynolds number.
|0 http://id.loc.gov/authorities/subjects/sh85113557
|
650 |
|
0 |
|a Transonic wind tunnels.
|0 http://id.loc.gov/authorities/subjects/sh85136997
|
650 |
|
0 |
|a Wall pressure (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh85144916
|
650 |
|
0 |
|a Boundary layer.
|0 http://id.loc.gov/authorities/subjects/sh85016095
|
650 |
|
7 |
|a Airfoils.
|2 nasat
|
650 |
|
7 |
|a Reynolds number.
|2 nasat
|
650 |
|
7 |
|a Transonic wind tunnels.
|2 nasat
|
650 |
|
7 |
|a Mach number.
|2 nasat
|
650 |
|
7 |
|a Boundary layers.
|2 nasat
|
650 |
|
7 |
|a Aerofoils
|x Testing.
|2 fast
|0 (OCoLC)fst00798250.
|
650 |
|
7 |
|a Boundary layer.
|2 fast
|0 (OCoLC)fst00837095.
|
650 |
|
7 |
|a Reynolds number.
|2 fast
|0 (OCoLC)fst01096833.
|
650 |
|
7 |
|a Transonic wind tunnels.
|2 fast
|0 (OCoLC)fst01154888.
|
650 |
|
7 |
|a Wall pressure (Aerodynamics)
|2 fast
|0 (OCoLC)fst01170116.
|
655 |
|
7 |
|a Statistics.
|2 fast
|0 (OCoLC)fst01423727.
|
710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch,
|e issuing body.
|0 http://id.loc.gov/authorities/names/n78091122
|
710 |
2 |
|
|a Langley Research Center.
|0 http://id.loc.gov/authorities/names/n79134855
|1 http://isni.org/isni/0000000406376754
|
776 |
0 |
8 |
|i Print version:
|a Jenkins, Renaldo V
|t R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
|w (OCoLC)36803025.
|
776 |
0 |
8 |
|i Microfiche version:
|a Jenkins, Renaldo V
|t R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
|w (OCoLC)56605234.
|
830 |
|
0 |
|a NASA technical paper ;
|v 2565.
|0 http://id.loc.gov/authorities/names/n42017381
|
856 |
4 |
0 |
|u https://purl.fdlp.gov/GPO/gpo105897
|z Online Access
|
907 |
|
|
|a .b101682992
|b 06-12-23
|c 08-08-18
|
944 |
|
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|a MARS - RDA ENRICHED
|
998 |
|
|
|a web
|b 08-08-18
|c -
|d m
|e -
|f eng
|g dcu
|h 0
|i 2
|
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|
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|a bslw22/23 : jun : ess (never sent)
|
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|s b28f2b31-6150-54b6-be30-24e062cb8090
|
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f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Online
|c Online
|d Online
|e NAS 1.60:2565
|h Superintendent of Documents classification
|i web
|n 1
|