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|a NAS 1.60:2565
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| 099 |
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|a Online Government Document
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| 100 |
1 |
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|a Jenkins, Renaldo V.,
|e author.
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| 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.
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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 computer
|b c
|2 rdamedia
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| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
1 |
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|a NASA/TP ;
|v 2565
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| 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.
|
| 536 |
|
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|a Langley Research Center
|d 505-61-01-02
|d L-16066
|
| 588 |
|
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|a Description based on online resource, PDF version; title from title page (NASA, viewed July 16, 2018).
|
| 650 |
|
7 |
|a Airfoils.
|2 nasat
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| 650 |
|
7 |
|a Reynolds number.
|2 nasat
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| 650 |
|
7 |
|a Transonic wind tunnels.
|2 nasat
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| 650 |
|
7 |
|a Mach number.
|2 nasat
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| 650 |
|
7 |
|a Boundary layers.
|2 nasat
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| 650 |
|
0 |
|a Aerofoils
|x Testing
|v Statistics.
|
| 650 |
|
0 |
|a Reynolds number.
|
| 650 |
|
0 |
|a Transonic wind tunnels.
|
| 650 |
|
0 |
|a Wall pressure (Aerodynamics)
|
| 650 |
|
0 |
|a Boundary layer.
|
| 650 |
|
7 |
|a Aerofoils
|x Testing.
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|0 (OCoLC)fst00798250
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| 650 |
|
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|a Boundary layer.
|2 fast
|0 (OCoLC)fst00837095
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| 650 |
|
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|a Reynolds number.
|2 fast
|0 (OCoLC)fst01096833
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| 650 |
|
7 |
|a Transonic wind tunnels.
|2 fast
|0 (OCoLC)fst01154888
|
| 650 |
|
7 |
|a Wall pressure (Aerodynamics)
|2 fast
|0 (OCoLC)fst01170116
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| 655 |
|
7 |
|a Statistics.
|2 fast
|0 (OCoLC)fst01423727
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| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch,
|e issuing body.
|
| 710 |
2 |
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|a Langley Research Center.
|
| 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:
|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.
|
| 856 |
4 |
0 |
|z CONNECT
|u https://purl.fdlp.gov/GPO/gpo105897
|t 0
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|b 06-10-21
|c 12-13-19
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|a Middle Tennessee State University
|b Main
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|d Electronic Resources
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|h Library of Congress classification
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