15th Applied Aerodynamics Conference 1997
DOI: 10.2514/6.1997-2298
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Experimental investigation of the flight of a sphere in weakly ionized air

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Cited by 18 publications
(11 citation statements)
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“…Based on this, a model for the thermophoretic force was developed for a wide variety of Knudsen numbers as given by Eqs. (31)(32)(33). This model agrees well with resolved-surface simulations and experimental data while tending to the correct theoretical limits, but does not account for heat or mass transfer effects.…”
Section: Discussionsupporting
confidence: 77%
“…Based on this, a model for the thermophoretic force was developed for a wide variety of Knudsen numbers as given by Eqs. (31)(32)(33). This model agrees well with resolved-surface simulations and experimental data while tending to the correct theoretical limits, but does not account for heat or mass transfer effects.…”
Section: Discussionsupporting
confidence: 77%
“…Given this fact, we cannot claim that we have presented the complete picture of diffusion in NiAl, even though we believe that the most important mechansims have been captured. The ongoing molecular-dynamics simulations 46 have only revealed three types of Ni vacancy jumps: NNN jumps, ͓110͔ 6JCs implemented by three two-atom transitions, and two-atom ͓111͔ jumps. The latter are short-lived and reverse after less than a picosecond.…”
Section: Discussionmentioning
confidence: 99%
“…46 An additional verification is essential since NEB calculations are based on a choice of the initial and final states of every atomic transition. The NEB method, therefore, can never guarantee that some unanticipated transitions are not missed in the calculations.…”
Section: Discussionmentioning
confidence: 99%
“…The hypersonic flight literature documents a number of efforts to develop such analyses, including those for aerodynamics (References [7,8]) and propulsion (References [9,10]). Meanwhile, several more efforts seek experimental solutions, as described in References [11][12][13][14]. Yet Blankson et al discuss the "inability of ground facilities to generate hypersonic test data at real flight conditions for validating design tools" [15].…”
Section: Figurementioning
confidence: 99%