Publication Date:
2019-07-12
Description:
The take-off stability characteristics of a Consolidated Vultee Aircraft Corporation Skate 7 seaplane were determined in the Langley tank no. 2. Trim limits of stability, trim tracks, and elevator limits of stability are presented.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-SL9D28a
Format:
application/pdf
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