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01833nam a2200325 i 4500 |
| 001 |
98521e28-9797-4209-bf06-c5a501961594 |
| 005 |
20240729000000.0 |
| 008 |
780901s1978 dcua b f000 0 eng d |
| 035 |
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|a (NcD)002843615DUK01
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| 035 |
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|a (OCoLC)04204434
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| 037 |
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|b 22161
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| 040 |
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|b eng
|c GPO
|d MvI
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| 074 |
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|a 830-H-15 (MF)
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| 086 |
0 |
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|a NAS 1.60:1151
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| 100 |
1 |
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|a Prust, Herman W
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| 245 |
1 |
0 |
|a Two-dimensional cold-air cascade study of a film-cooled turbine stator blade :
|b IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter-(0.030-in.-) (0.030-in.-) diameter holes having streamwise ejection angles /
|c Herman W. Prust, Jr. ; Lewis Research Center
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| 260 |
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|a [Washington] :
|b National Aeronautics and Space Administration, Scientific and Technical Information Office ;
|a Springfield, Va. :
|b for sale by the National Technical Information Service,
|c 1978
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| 300 |
|
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|a 27 p. :
|b ill. ;
|c 27 cm
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
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| 337 |
|
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|a unmediated
|b n
|2 rdamedia
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| 338 |
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|a volume
|b nc
|2 rdacarrier
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| 490 |
1 |
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|a NASA technical paper ;
|v 1151
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| 500 |
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|a Issued Mar. 1978
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| 504 |
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|a Includes bibliographical references
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| 650 |
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0 |
|a Turbines
|x Blades
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| 710 |
1 |
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|a United States
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office.
|
| 710 |
2 |
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|a Lewis Research Center
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| 830 |
|
0 |
|a NASA technical paper ;
|v 1151
|
| 999 |
1 |
0 |
|i 98521e28-9797-4209-bf06-c5a501961594
|l 990028436150108501
|s US-NCD
|m two_dimensional_cold_air_cascade_study_of_a_film_cooled_turbine_stator_____1978_______natioa________________________________________prust__herman_w____________________nas_1_60_1151p
|
| 999 |
1 |
1 |
|l 990028436150108501
|s ISIL:US-NCD
|t BKS
|a PERKN PKM1
|b HBFY-3564-00001
|c NAS 1.60:1151
|d 3
|x BOOK
|y 23662568520008501
|p UNLOANABLE
|