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02128nam a2200349Ia 4500 |
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4adf4b81-9d54-4d39-a232-3dfb12450ff6 |
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20230617000000.0 |
| 008 |
101208s1958 dcua tb f000 0 eng d |
| 035 |
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|a (OCoLC-I)805557693
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| 035 |
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|a (OCoLC-M)690692926
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| 040 |
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|a LHL
|c LHL
|d LHL
|d UtOrBLW
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| 086 |
0 |
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|a Y 3.N 21/5:6/4174
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| 100 |
1 |
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|a Wiggins, James W
|? UNAUTHORIZED
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| 245 |
1 |
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|a Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. :
|b Taper-ratio series /
|c James W. Wiggins and Paul G. Fournier
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| 260 |
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|a Washington :
|b National Advisory Committee for Aeronautics,
|c [1958]
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| 300 |
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|a 25 p. :
|b ill ;
|c 27 cm
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| 490 |
1 |
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|a Technical note / National Advisory Committee for Aeronautics ;
|v 4174
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| 500 |
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|a NACA TN No. 4174
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| 504 |
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|a Includes bibliographical references
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| 520 |
3 |
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|a An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of variations in taper ratio within the range of 0.3 to 1.0 on the static lateral stability characteristics at high subsonic speeds of wing-fuselage combinations having wings of 45 degrees sweepback at the quarter-chord line and an aspect ratio of 4
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|a Copy 1 bound with 4165
|c 9120278 (parent record's ckey)
|b 36105024832409 (item id)
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| 596 |
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|a 31
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| 650 |
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|a Aerodynamics, Supersonic
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| 650 |
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|a Airplanes
|x Fuselage
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| 650 |
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0 |
|a Airplanes
|x Wings
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| 650 |
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|a Stability of airplanes, Lateral
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| 650 |
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0 |
|a Wind tunnel testing
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| 700 |
1 |
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|a Fournier, Paul G
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| 710 |
1 |
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|a United States
|b National Advisory Committee for Aeronautics.
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| 830 |
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0 |
|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 4174
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| 999 |
1 |
0 |
|i 4adf4b81-9d54-4d39-a232-3dfb12450ff6
|l a9120295
|s US-CST
|m wind_tunnel_investigation_of_the_static_lateral_stability_characterist_____1958_______natioa________________________________________wiggins__james_w___________________y_3_n_21_5_6_4174p
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| 999 |
1 |
1 |
|l a9120295
|s ISIL:US-CST
|t BKS
|a SAL3 SEE-OTHER
|b 9120295-1001
|c NACA TN 4174
|d ALPHANUM
|x STKS-MONO
|y 9120295-1001
|p UNLOANABLE
|