Effects of porous rings on the aerodynamic characteristics of a sphere
A number of design concepts were tested statically and dynamically to determine their ability to improve the stability characteristics and drag coefficient of a sphere. The most successful configuration tested was a thick (0.05d) porous ring, equatorially located. Results of static tests measuring a...
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Veröffentlicht in: | Journal of spacecraft and rockets 1975-09, Vol.12 (9), p.572-574 |
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Format: | Artikel |
Sprache: | eng |
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