Technical Paper

Prediction of the Laminar-to-turbulent Transition Position on a Helicopter Rotor Blade with Cyclic Pitch Variation

F-0079-2023-18128

5/16/2023

Event
Vertical Flight Society 79th Annual Forum and Technology Display
Authors
Francois Richez ONERA - The French Aerospace Lab
Rohit Jain US Army CCDC AvMC
Abstract
Content

Meta Tags
Topics
Propellers and rotors
Pitch
Affiliated or Co-Author
ONERA - The French Aerospace Lab
US Army CCDC AvMC
Details
Pages
18
Citation
Richez, F. and Jain, R., "Prediction of the Laminar-to-turbulent Transition Position on a Helicopter Rotor Blade with Cyclic Pitch Variation," Vertical Flight Society 79th Annual Forum and Technology Display, West Palm Beach, Florida, May 16, 2023, .
Additional Details
Publisher
The Vertical Flight Society
Published
5/16/2023
Product Code
F-0079-2023-18128
Content Type
Technical Paper
Language
English