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|a (OCoLC)ocn663650967
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|a (OCoLC)663650967
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|a LHL
|b eng
|c LHL
|d LHL
|d OCLCF
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|a COD9
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| 086 |
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|a Y 3.N 21/5:6/2146
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| 100 |
1 |
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|a Ribner, H. S.
|q (Herbert S.),
|d 1913-
|0 http://id.loc.gov/authorities/names/no97049676
|1 http://isni.org/isni/0000000078935819.
|
| 245 |
1 |
0 |
|a On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream /
|c Herbert S. Ribner.
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| 260 |
|
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1950.
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| 300 |
|
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|a 27 pages :
|b illustrations ;
|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. Technical Note ;
|v no. 2146.
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| 500 |
|
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|a "August 1950."
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| 500 |
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|a NACA TN Number 2146.
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| 504 |
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|a Includes bibliographical references.
|
| 520 |
3 |
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|a The principal effect of subsonic trailing edges on the damping in roll and pitch of thin sweptback wings in a supersonic stream is evaluated in the form of approximate correction terms. These terms are to be added to the corresponding expressions obtained when the trailing-edge disturbances are ignored. Application is limited to plan forms and Mach numbers for which the trailing-edge disturbance does not extend beyond the leading edge and for which the area of mutual tip-trailing-edge interference is not large.
|
| 583 |
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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 Airplanes
|x Wings, Swept-back.
|0 http://id.loc.gov/authorities/subjects/sh85002928.
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic.
|0 http://id.loc.gov/authorities/subjects/sh85001297.
|
| 650 |
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0 |
|a Rolling (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh85114890.
|
| 650 |
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0 |
|a Trailing edges (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh2003006701.
|
| 650 |
|
7 |
|a Aerodynamics, Supersonic.
|2 fast
|0 (OCoLC)fst00798221.
|
| 650 |
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7 |
|a Airplanes
|x Wings, Swept-back.
|2 fast
|0 (OCoLC)fst00803560.
|
| 650 |
|
7 |
|a Rolling (Aerodynamics)
|2 fast
|0 (OCoLC)fst01099689.
|
| 650 |
|
7 |
|a Trailing edges (Aerodynamics)
|2 fast
|0 (OCoLC)fst01154417.
|
| 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 2146.
|0 http://id.loc.gov/authorities/names/no2009017392.
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| 907 |
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|b 08-13-20
|c 11-18-16
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|b 10-11-17
|c 11-18-16
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|a MARS - RDA ENRICHED
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| 907 |
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|a .b89488325
|b 01-05-17
|c 11-18-16
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|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Offsite
|d PASCAL Offsite
|e Y 3.N 21/5:6/2146
|h Superintendent of Documents classification
|i document
|m P203170903031
|n 1
|
