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101019e195401 ohua bt f000 0 eng d |
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20231211205402.3 |
| 035 |
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|a (OCoLC)ocn670572860
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| 035 |
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|a (OCoLC)670572860
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| 040 |
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|a LHL
|b eng
|c LHL
|d LHL
|d OCLCF
|d OCLCO
|d OCLCQ
|d COD
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| 049 |
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|a COD9
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| 086 |
0 |
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|a Y 3.N 21/5:6/3115
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| 100 |
1 |
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|a MacNeal, R.
|q (Richard)
|0 http://id.loc.gov/authorities/names/n86816209
|1 http://isni.org/isni/0000000373948022.
|
| 245 |
1 |
0 |
|a Analysis of sweptback wings on Cal-Tech analog computer /
|c Richard H. MacNeal and Stanley U. Benscoter.
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| 260 |
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1954.
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| 300 |
|
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|a 80 pages :
|b illustrations, tables ;
|c 28 cm.
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| 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 National Advisory Committee for Aeronautics ;
|v no. 3115.
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| 500 |
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|a "January 1954."
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| 500 |
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|a NACA TN Number 3115.
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| 504 |
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|a Includes bibliographical references.
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| 520 |
3 |
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|a Using the Cal-Tech analog computer, structural analyses have been made on two 45 degree swept wings of aspect ratio 3. One of these has a constant depth and the other has a constant biconvex cross section in planes parallel to the air stream. The wings extend through the fuselage and are rigidly supported along two iines at the faces of the fuselage.
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| 520 |
3 |
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|a Deflections and all internal forces have been calculated for concentrated static loads. Vibration modes are also presented. The effects of neglecting shearing strains in the ribs and spars and also of assuming the ribs to be rigid have been investigated by modifying the electric circuits to correspond to these simplifications.
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| 583 |
1 |
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|a committed to retain
|c 20230101
|d 20480101
|5 CoU
|f Alliance Shared Trust
|u https://www.coalliance.org/shared-print-archiving-policies.
|
| 650 |
|
0 |
|a Electronic analog computers.
|0 http://id.loc.gov/authorities/subjects/sh85042250.
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| 650 |
|
0 |
|a Airplanes
|x Wings, Swept-back.
|0 http://id.loc.gov/authorities/subjects/sh85002928.
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| 650 |
|
0 |
|a Structural analysis (Engineering)
|0 http://id.loc.gov/authorities/subjects/sh85129216.
|
| 650 |
|
7 |
|a Airplanes
|x Wings, Swept-back.
|2 fast
|0 (OCoLC)fst00803560.
|
| 650 |
|
7 |
|a Electronic analog computers.
|2 fast
|0 (OCoLC)fst00906756.
|
| 650 |
|
7 |
|a Structural analysis (Engineering)
|2 fast
|0 (OCoLC)fst01135602.
|
| 700 |
1 |
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|a Benscoter, Stanley Urner.
|0 http://id.loc.gov/authorities/names/no2017028536.
|
| 710 |
1 |
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|a United States.
|b National Advisory Committee for Aeronautics.
|0 http://id.loc.gov/authorities/names/n79060141
|1 http://isni.org/isni/0000000106642010.
|
| 830 |
|
0 |
|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 3115.
|0 http://id.loc.gov/authorities/names/no2009017392.
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| 907 |
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|a .b90350157
|b 08-13-20
|c 02-14-17
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|a .b90350157
|b 11-15-19
|c 02-14-17
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| 944 |
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|a MARS - RDA ENRICHED
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| 907 |
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|a .b90350157
|b 05-17-17
|c 02-14-17
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| 907 |
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|b 02-14-17
|c 02-14-17
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| 952 |
f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Offsite
|d PASCAL Offsite
|e Y 3.N 21/5:6/3115
|h Superintendent of Documents classification
|i document
|m P204060505029
|n 1
|
