Publication Date:
2019-07-11
Description:
A supplementary investigation on the stabilization of the Jettisonable nose section of the X-2 airplane has been conducted in the Langley 20-foot free-spinning tunnel. It was found that the nose section could be stabilized by the addition of curved fins which could be folded against the fuselage for normal flight.
Keywords:
Aerodynamics
Type:
NACA-RM-L9F22
Format:
application/pdf
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