Preliminary Results of Flight Tests of a Conventional Three-Blade Propeller at High Speeds

[摘要] As part of the program of flight tests of airplane propellers to determine compressibility effects at high speeds, preliminary flights have been made with a conventional three-blade propeller (Hamilton Standard 3155-6) on a Bell YP-39 airplane. This preliminary report presents the high-speed data obtained thus far with a brief analysis of the results.

[发布日期] 1942-04-01

[学科分类] 航空航天科学