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|a Y 3.N 21/5:6/2285
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|a Y 3.N 21/5:6/2285
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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.
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|a Damping in roll of cruciform and some related delta wings at supersonic speeds /
|c Herbert S. Ribner.
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1951.
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|a 43 pages :
|b illustrations ;
|c 28 cm.
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|a text
|b txt
|2 rdacontent.
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|a unmediated
|b n
|2 rdamedia.
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|a volume
|b nc
|2 rdacarrier.
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|a National Advisory Committee for Aeronautics. Technical Note ;
|v no. 2285.
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|a "February 1951."
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|a NACA TN Number 2285.
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|a Includes bibliographical references.
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|a The damping in roll of cruciform delta wings in supersonic flow has been evaluated by means of small-disturbance (linearized) wing theory; both subsonic and supersonic component stream velocities normal to the leading edges have been considered. In addition, some known two-dimensional results for rotating multibladed laminae have been applied to obtain the loading when the number of panels is changed from four to an arbitrary number, under the restriction of low aspect ratio; the damping in roll has been determined explicitly for three panels. Finally, the damping for an inifinite number of panels has been evaluated without restriction as to aspect ratio or Mach number.
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|a will digitize
|c 20121201
|z Queued for digitization December 1, 2012
|2 pda
|5 miu.
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|a Airplanes
|x Wings, Triangular.
|0 http://id.loc.gov/authorities/subjects/sh85002930.
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|a Rolling (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh85114890.
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|a Aerodynamics, Supersonic.
|0 http://id.loc.gov/authorities/subjects/sh85001297.
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|a Aerodynamics, Supersonic.
|2 fast
|0 (OCoLC)fst00798221.
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|a Airplanes
|x Wings, Triangular.
|2 fast
|0 (OCoLC)fst00803564.
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|a Rolling (Aerodynamics)
|2 fast
|0 (OCoLC)fst01099689.
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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.
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|a Technical report archive and image library.
|0 http://id.loc.gov/authorities/names/no2008179973.
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|i Online version:
|a Ribner, H.S. (Herbert S.), 1913-
|t Damping in roll of cruciform and some related delta wings at supersonic speeds.
|d Washington, D.C. : National Advisory Committee for Aeronautics, 1951
|w (OCoLC)885453150.
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| 830 |
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v 2285.
|0 http://id.loc.gov/authorities/names/no2009017392.
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|u https://www.hathitrust.org/
|z Search for the full-text version of this title in HathiTrust
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|a University of Colorado Boulder
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|e Y 3.N 21/5:6/2285
|h Superintendent of Documents classification
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