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by
Koessler, Jeffrey H., author.
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-Serret equations. A series of dynamic soaring steady-state scenarios are presented and used to amplify the spatial
by
Chati, Yashovardhan Sushil, author.
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developed for each aircraft type and for each of the flight phases. The Bayesian technique of Gaussian
by
Ning, Zhe, author. (orcid)0000-0002-4884-5251
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). The sound measurements were conducted inside of the anechoic chamber located in the aerospace
by
Manar, Field Hogan, author.
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proposal of a new relationship between the wake state and the leading edge circulation production, termed
by
Holloway, John Charles, author.
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state in a finite time that is independent of initial conditions and freely prescribed by the user. The
by
Yeung, Kan Kan, author.
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-stop and regenerative braking systems, where LABs mainly undergo partial state of charge (PSoC) operation
by
Callender, William Bryan, author.
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. This rig has subsequently been used to advance the understanding of two state-of-the-art jet noise
by
Alkhozam, Abdullah M., author.
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measurements. In both facilities dynamic and steady state or static measurements were made on half delta wing
by
Edi, Prasetyo, author.
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front of the recovery point. To identify the drag reductions by the applications of combined HLFC
by
Karni, S., author.
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conditions must be specified at the artificial boundary for well-posedness of the truncated problem. They
by
Antony, Thomas, author.
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illustrated by the various examples in this dissertation, it has made significant advances in automating the
by
Chap, Andrew Mark, author. (orcid)0000-0002-8513-3632
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Alıntı:
developed to investigate the effect of ions on an electrostatically and magnetically confined electron

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