Effect of Crossflow Transition on the Pressure-Sensitive-Paint Rotor in Hover-Reference-Cited by-同舟云学术

Effect of Crossflow Transition on the Pressure-Sensitive-Paint Rotor in Hover

Published:2022-01 Issue:1 Volume:59 Page:29-46
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Carnes Jared A.¹,Coder James G.¹

Affiliation:

1. University of Tennessee, Knoxville, Tennessee 37996

Funder

Penn State Vertical Lift Research Center of Excellence

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036121

Reference29 articles.

1. BalchD. T.LombardiJ. “Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interactions in Hover. Vol. I–Text and Figures,” NASA CR-177336, 1985.

2. Comparison of Computational Fluid Dynamics Hover Predictions on the S-76 Rotor

3. Navier-Stokes Analysis of Helicopter Rotor Aerodynamics in Hover and Forward Flight

4. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes

5. Improved Rotor Hover Predictions Using Advanced Turbulence Modeling

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