Publikationsdatum:
2019-06-28
Beschreibung:
For several years, the TAD2 computer program has been used to calculate the aerodynamic properties of sounding rockets. This program was limited, however, in that a maximum of two fin sets could be accommodated analytically. In addition, the roll moment coefficients did not consider downwash effects. Techniques are developed and equations derived for the expansion of capability to include three fin sets. The effects of downwash on the roll moment coefficients are also treated analytically for two and three stage rockets.
Schlagwort(e):
AERODYNAMICS
Materialart:
AIAA PAPER 86-2528
Format:
text
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