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991126m19969999dcu b f000 0 eng d |
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|a (OCoLC)ocm42890754
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|a 19960047488 (v.2)
|b NASA
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|a 19960047655 (v.2)
|b NASA
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|a GPO
|b eng
|c GPO
|d SYB
|d OCLCQ
|d OCLCO
|d GPO
|d MvI
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|a COD9
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|a 0830-D (MF)
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|a NAS 1.15:4645
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|a NAS 1.15:4645
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|a Chu, Julio.
|0 http://id.loc.gov/authorities/names/n81030362.
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|a Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges
|h [microform] /
|c Julio Chu and James M. Luckring.
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|a Hampton, Va. :
|b National Aeronautics and Space Administration, Langley Research Center ;
|a [Springfield, Va.] :
|b [National Technical Information Service, distributor],
|c [1996-]
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|a volumes.
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|a text
|b txt
|2 rdacontent.
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|a microform
|b h
|2 rdamedia.
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|a microfiche
|b he
|2 rdacarrier.
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|a NASA technical memorandum ;
|v 4645.
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|a Shipping list number: 98-0799-M (volume 2)
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1 |
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|a v. 2. Small-radius leading edge.
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|a Microfiche.
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,
|d 1997-].
|e <1> microfiche.
|
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|a Wind tunnel
|x Examinations.
|
650 |
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|a Airplanes
|x Wings, Triangular.
|0 http://id.loc.gov/authorities/subjects/sh85002930.
|
650 |
|
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|a Reynolds number.
|0 http://id.loc.gov/authorities/subjects/sh85113557.
|
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|a Mach number.
|0 http://id.loc.gov/authorities/subjects/sh85079305.
|
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|a Aerodynamics.
|0 http://id.loc.gov/authorities/subjects/sh85001295.
|
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7 |
|a Wind tunnel tests.
|2 nasat.
|
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|
7 |
|a Delta wings.
|2 nasat.
|
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|
7 |
|a Leading edges.
|2 nasat.
|
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|
7 |
|a Reynolds number.
|2 nasat.
|
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|
7 |
|a Mach number.
|2 nasat.
|
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|
7 |
|a Vortices.
|2 nasat.
|
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7 |
|a Slender wings.
|2 nasat.
|
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|
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|a Pressure distribution.
|2 nasat.
|
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|a Subsonic speed.
|2 nasat.
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1 |
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|a Luckring, James M.
|0 http://id.loc.gov/authorities/names/n82083098
|1 http://isni.org/isni/0000000033639047.
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2 |
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|a Langley Research Center.
|0 http://id.loc.gov/authorities/names/n79134855
|1 http://isni.org/isni/0000000406376754.
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|a Small-radius leading edge.
|
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0 |
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|i Print version:
|a Chu, Julio.
|t Experimental surface pressure data obtained on 65̊ delta wing across reynolds number and mach number ranges
|w (OCoLC)51039329.
|
776 |
0 |
8 |
|i Online version:
|a Chu, Julio.
|t Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges
|w (OCoLC)945978511.
|
830 |
|
0 |
|a NASA technical memorandum ;
|v 4645.
|0 http://id.loc.gov/authorities/names/n83707893.
|
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|a .b31067335
|b 04-05-22
|c 01-18-00
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|a gov
|b 02-10-07
|c -
|d m
|e -
|f eng
|g dcu
|h 0
|i 3
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|a .b31067335
|b 05-15-20
|c 01-18-00
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|a MARS - RDA ENRICHED
|
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f |
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|i 0365b654-6129-5af6-9d5d-3816518a6385
|s cee22eba-a37a-5ae0-9d33-e0e36d9e84c0
|
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f |
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|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Norlin
|d Norlin Library - Government Information - Microform
|e NAS 1.15:4645
|h Superintendent of Documents classification
|i document
|j vol.2
|n 1
|