W. J. Mulcay

Rotary balance data for a single engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 deg to 90 deg

W. J. Mulcay, R. Rose, 1980 .

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8 deg to 90 deg

J. Chu, W. J. Mulcay, 1980 .

Rotary balance data for a typical single-engine general aviation design for an angle of attack range of 8 deg to 90 deg. 1: Low wing model C. [wind tunnel tests

W. J. Mulcay, R. A. Rose, W. Mulcay, 1980 .