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| 001 |
b5143a70-cafd-4522-8aa2-6d8b7b9e4dd4 |
| 005 |
20240707000000.0 |
| 008 |
890103s1985 dcua btb f000 0 eng d |
| 035 |
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|a (OCoLC)18959258
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| 037 |
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|a N 85-34355
|b NASA
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| 040 |
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|a GPO
|c GPO
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| 049 |
|
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|a MNUK
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| 050 |
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4 |
|a TL521.3.T4
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| 074 |
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|a 830-D (microfiche)
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| 086 |
0 |
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|a NAS 1.15:86389
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| 099 |
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|a NAS 1.15:86389
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| 100 |
1 |
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|a Creel, Theodore R.
|
| 245 |
1 |
0 |
|a Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /
|c Theodore R. Creel, Jr., and Ivan E. Beckwith, Fang-Jenq Chen.
|
| 260 |
|
|
|a [Washington, D.C.] :
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch ;
|a [Springfield, Va.] :
|b [For sale by the National Technical Information Service],
|c 1985.
|
| 300 |
|
|
|a 1 volume :
|b illustrations ;
|c 28 cm.
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a microform
|b h
|2 rdamedia
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| 338 |
|
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|a microfiche
|b he
|2 rdacarrier
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| 490 |
1 |
|
|a NASA technical memorandum;
|v 86389
|
| 500 |
|
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|a Cover title.
|
| 500 |
|
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|a Distributed to depository libraries in microfiche.
|
| 500 |
|
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|a STAR category 34.
|
| 504 |
|
|
|a Bibliography: page 10.
|
| 533 |
|
|
|a Microfiche.
|b [Washington, D.C.? :
|c National Aeronautics and Space Administration],
|d 1985.
|e 1 microfiche ; 11 x 15 cm.
|
| 650 |
|
0 |
|a Supersonic wind tunnels.
|
| 650 |
|
0 |
|a Reynolds number.
|
| 650 |
|
0 |
|a Boundary layer noise.
|
| 700 |
1 |
|
|a Beckwith, Ivan E.
|
| 700 |
1 |
|
|a Chen, Fang-Jenq.
|
| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch.
|
| 830 |
|
0 |
|a NASA technical memorandum
|v 86389.
|
| 999 |
1 |
0 |
|i b5143a70-cafd-4522-8aa2-6d8b7b9e4dd4
|l 9927670000001701
|s US-MNU
|m nozzle_wall_roughness_effects_on_free_stream_noise_and_transition_in_t_____1985_______natioa________________________________________creel__theodore_r__________________nas_1_15_86389p
|