Prediction of the Laminar-to-turbulent Transition Position on a Helicopter Rotor Blade with Cyclic Pitch Variation
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- SKU # : F-0079-2023-18128 Aerodynamics
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Prediction of the Laminar-to-turbulent Transition Position on a Helicopter Rotor Blade with Cyclic Pitch Variation
Authors / Details:Francois Richez, ONERA - The French Aerospace Lab
Rohit Jain, US Army CCDC AvMC
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