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    Free-Spinning-Tunnel Tests of a 1/35-Scale Model of the Douglas XB-43 Airplane (1947)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: Spin tests have been performed in the Langley 20-foot free-spinning tunnel on a 1/35-scale model of the Douglas XB-43 airplane. The spin and recovery characteristics were determined for several loading conditions of the airplane. The effects of installing a dorsal fin and of installing a ventral fin were investigated. Emergency escape of the crew was simulated and the stick and rudder pedal forces necessary to effect recoveries on the airplane were determined.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-L7G01
    Format: application/pdf
    Location Call Number Expected Availability
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