TY  - RPRT
TI  - Forced Response Aeromechanics Analysis in MATLAB®-Based Environment Code With Application to Distortion-Tolerant Fan R24 Blade Geometry
AU  - Austin J. Schemmel
PY  - 2024
UR  - https://ntrs.nasa.gov/citations/20240000075
ID  - 20240000075
ER  -