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03048nam a2200697Ii 4500 |
| 001 |
761260747 |
| 003 |
OCoLC |
| 005 |
20180615105023.0 |
| 006 |
m o d f |
| 007 |
cr un||||a|a|| |
| 008 |
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| 040 |
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|a OCLCE
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|d OCLCQ
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|d GPO
|d MvI
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| 049 |
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|a COM7
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| 074 |
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|a 0830-H-15 (online)
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| 086 |
0 |
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|a NAS 1.60:2430
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| 100 |
1 |
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|a Miller, David S.,
|e author.
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| 245 |
1 |
0 |
|a Lee-side flow over delta wings at supersonic speeds /
|c David S. Miller and Richard M. Wood.
|
| 264 |
|
1 |
|a Washington, D.C. :
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c June 1985.
|
| 300 |
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|a 1 online resource (iii, 150 pages) :
|b illustrations.
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| 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 2430.
|
| 500 |
|
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|a "June 1985."
|
| 500 |
|
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|a Prepared at Langley Research Center.
|
| 500 |
|
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|a CRDP Program record.
|
| 504 |
|
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|a Includes bibliographical references (page 150).
|
| 513 |
|
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|a Technical paper.
|
| 536 |
|
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|a Langley Research Center
|d 505-43-23-02
|d L-15888.
|
| 588 |
|
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|a Description based on online resource, PDF version; title from title page (NASA, viewed June 15, 2018).
|
| 650 |
|
7 |
|a Delta wings.
|2 nasat.
|
| 650 |
|
7 |
|a Flow characteristics.
|2 nasat.
|
| 650 |
|
7 |
|a Leading edges.
|2 nasat.
|
| 650 |
|
7 |
|a Flow visualization.
|2 nasat.
|
| 650 |
|
7 |
|a Pressure measurement.
|2 nasat.
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic.
|
| 650 |
|
0 |
|a Airplanes
|x Wings, Triangular.
|
| 650 |
|
0 |
|a Vortex-motion.
|
| 650 |
|
0 |
|a Leading edges (Aerodynamics)
|
| 650 |
|
7 |
|a Aerodynamics, Supersonic.
|2 fast.
|
| 650 |
|
7 |
|a Airplanes
|x Wings, Triangular.
|2 fast.
|
| 650 |
|
7 |
|a Leading edges (Aerodynamics)
|2 fast.
|
| 650 |
|
7 |
|a Vortex-motion.
|2 fast.
|
| 655 |
|
7 |
|a Technical reports.
|2 lcgft.
|
| 700 |
1 |
|
|a Wood, Richard M.,
|e author.
|
| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch,
|e issuing body.
|
| 710 |
2 |
|
|a Langley Research Center.
|
| 776 |
0 |
8 |
|i Print version:
|a Miller, David S
|t Lee-side flow over delta wings at supersonic speeds
|w (OCoLC)26776650.
|
| 776 |
0 |
8 |
|i Microfiche:
|a Miller, David S
|t Lee-side flow over delta wings at supersonic speeds
|w (OCoLC)56538141.
|
| 830 |
|
0 |
|a NASA technical paper ;
|v 2430.
|
| 856 |
4 |
0 |
|u https://purl.fdlp.gov/GPO/gpo93622
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|a MARCIVE Overnight, in 2023.01
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| 948 |
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|a MARCIVE Comp, 12/2021
|
| 948 |
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|a MARCIVE Q3&4 2018
|
| 995 |
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|a Loaded with m2btab.ltiac in 2023.01
|
| 995 |
|
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|a Loaded with m2btab.ltiac in 2021.12
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| 995 |
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|a Loaded with m2btab.ltiac in 2019.01
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| 995 |
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|a Loaded with m2btab.msgov7 in 2018.08
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