High loading low speed fan study. Part 1 - Design
Airfoil design, structural analysis, and aerodynamic characteristics of low-speed compressor fan
Keenan, M. J.↗
Engineering topics
Monsarrat, N. T.
Publications and source records attributed to Monsarrat, N. T..
Single-stage evaluation of highly-loaded high-Mach-number compressor stages
Aerodynamical and mechanical single stage evaluation of highly loaded, high Mach number compressor stages
Keenan, M. J.↗
Experimental Evaluation of Transonic Stators Preliminary Analysis and Design Report
A flow-generating rotor has been designed under NASA contract NAS3-7614 to enable three transonic stators to be tested. The stators were designed by NASA in conjunction with the Contractor. Design analyses were conducted and the results indicate that the rotor will produce the required inlet flow to the stators. Structural and vibration analyses indicate that resonances and critical speeds occur outside the operating range and that the component stresses will be well within the capabilities of the materials used. Design details of the flow generation rotor and the three transonic stators are presented.
INLET FLOW↗