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| LEADER |
00000cam a2200000 a 4500 |
| 001 |
58ae85c3-5935-4522-8401-62359dd4858d |
| 005 |
20240707000000.0 |
| 008 |
821020s1982 dcua b f000 0 eng d |
| 035 |
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|a (OCoLC)8882932
|
| 040 |
|
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|a GPO
|c GPO
|
| 049 |
|
|
|a MNUK
|
| 050 |
|
4 |
|a TL574.S6
|
| 074 |
|
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|a 830-H-14 (microfiche)
|
| 086 |
0 |
|
|a NAS 1.26:3516
|
| 099 |
|
|
|a NAS 1.26:3516
|
| 100 |
1 |
|
|a Barnhart, Billy.
|
| 245 |
1 |
0 |
|a Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8° to 90° /
|c Billy Barnhart ; prepared for Langley Research Center under contract NAS1-16205.
|
| 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 1982.
|
| 300 |
|
|
|a 377 pages :
|b illustrations ;
|c 28 cm.
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a unmediated
|b n
|2 rdamedia
|
| 338 |
|
|
|a volume
|b nc
|2 rdacarrier
|
| 490 |
1 |
|
|a NASA contractor report;
|v 3516
|
| 500 |
|
|
|a "May 1982"--Cover.
|
| 500 |
|
|
|a Subject Category 02.
|
| 504 |
|
|
|a Includes bibliographical references.
|
| 650 |
|
0 |
|a Spin (Aerodynamics)
|
| 650 |
|
0 |
|a Eagle (Jet fighter plane)
|x Testing.
|
| 650 |
|
0 |
|a Wind tunnels.
|
| 710 |
1 |
|
|a United States.
|b Aeronautics and Space Administration.
|b Scientific and Technical Information Branch.
|
| 710 |
2 |
|
|a Langley Research Center.
|
| 830 |
|
0 |
|a NASA contractor report ;
|v 3516.
|
| 999 |
1 |
0 |
|i 58ae85c3-5935-4522-8401-62359dd4858d
|l 9929255800001701
|s US-MNU
|m rotary_balance_data_for_an_f_15_model_with_fuel_tanks_for_an_angle_of______1982_______natioa________________________________________barnhart__billy____________________nas_1_26_3516p
|