Effect of Camber on the Trimmed Lift Capability of a Close-Coupled Canard-Wing Configuration

摘要

A close-coupled canard-wing configuration was tested in the Langley high-speed 7- by 10-foot tunnel at a Mach number of 0.30 to determine the effect of changing wing camber on the trimmed lift capability. Trimmed lift coefficients of near 2.0 were attained;however, the data indicated that the highest buffet-free trimmed lift coefficient attainable was approximately 1.30. The buffet data used in this inves¬tigation were qualitative in nature and gave no indication of buffet intensity. Thus, the trimmed lift coefficient of near 2.0 might be attainable if the buffet intensity was not too high. The data showed that there was approximately a 10-percent variation in drag coefficient, for different model configurations, at a given trimmed lift coefficient. Large increases in wing lift had only small effects on canard lift.