TY  - CONF

T1  - Application of Engineering Transition Models to an Isolated Helicopter Rotor in Hovering Flight

JO  - 43rd AIAA Aerospace Sciences Meeting and Exhibit

UR  - https://doi.org/10.2514/6.2005-467

PY  - 2005/01/10

AU  - Shaw S

AU  - Hill J

AU  - Qin N

ED  - 

DO  - DOI: 10.2514/6.2005-467

PB  - American Institute of Aeronautics and Astronautics

Y2  - 2025/11/03

ER  -