Compound rotorcraft can be a viable option to achieve moderately high speeds of 240 knots.
However, there is no systematic wind tunnel test data in the public domain to understand the …

This paper details the propeller analysis in forward flight to finalize the wind tunnel test
matrix of the thrust compounding rotorcraft model. First, the University of Maryland Advanced …

This paper focuses on the validation and investigation of interactional acoustics of a modern
wing and pusher propeller configuration, which was tested in the National Full-Scale …