Advanced Chinook Rotor Blade (ACRB)
Abstract
This effort designs, develops and performs contractor led component qualification for an improved rotor blade capability. This capability significantly increases lift capability, reduces Operation and Support (O&S) costs and is a form, fit replacement for the current blade, which will enable payload restoration to the ground force commander. Conduct additional flight testing to reduce risk for Engineering and Manufacturing Development (EMD) and validate Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) models.
Document Details
- Document Type
- Accomplishment
- Publication Date
- Oct 01, 2021
- Source ID
- 905914aaadd79444614db4a1ee002cde