Effect of afterbody configuration on damping coefficients for axisymmetric projectiles

Publisher
AMER INST AERONAUT ASTRONAUT
Issue Date
2004-11
Language
ENG
Keywords

TURBULENCE MODELS

Citation

JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.6, pp.1065 - 1068

ISSN
0022-4650
URI
http://hdl.handle.net/10203/6815
Appears in Collection
AE-Journal Papers(저널논문)
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