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Direct solution of the aeroelastic stability equations

descriptionPublicationkeyboard_double_arrow_right Article 01 Jul 1994 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Aircraft, volume 31, pages 979-981 (issn: 0021-8669, eissn: 1533-3868, Copyright policy )
Authors: Maher N. Bismarck-Nasr;

doi: 10.2514/3.46590

Direct solution of the aeroelastic stability equations

Abstract

Acknowledgments This research was sponsored, in part, by the National Aeronautics and Space Administration under Contract NAS118585. The author also acknowledges the assistance with using the CFL3D code and the various turbulence models made by Christopher Rumsey of NASA Langley Research Center. The experimental data was provided to NASA Langley Research Center by Frank Lynch of McDonnell Douglas Aerospace— Transport Aircraft Unit.

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This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
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popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
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