Inviscid Flow Analysis on Body of Revolution with Slender Cruciform Canted Delta Fins at Small Angle of Incidence.
TENNESSEE UNIV SPACE INST TULLAHOMA
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An analysis of the aerodynamic characteristics for a slender fin-body configuration at transonic speeds with an exhaust plume has been developed. Sample calculations for small combined angles of attack, yaw and fin cant, are presented. The analysis is limited to cases of subsonic fin leading edges.
- Fluid Mechanics