Scaling and Configuration Effects on Helicopter Rotor Hub Interactional Aerodynamics-Reference-Cited by-同舟云学术

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Scaling and Configuration Effects on Helicopter Rotor Hub Interactional Aerodynamics

Published:2017-09 Issue:5 Volume:54 Page:1692-1704
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Reich David¹,Willits Steven¹,Schmitz Sven¹

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

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.C034250

Reference25 articles.

1. Guidelines for Reducing Helicopter Parasite Drag

2. KeysC. N.RosensteinH. “Summary of Rotor Hub Drag Data,” NASA TR NASA CR-152080, 1978.

3. ChurchillG.HarringtonR. “Parasite-Drag Measurements of Five Helicopter Rotor Hubs,” NASA TM 1-21-59L, 1959.

4. Experimental investigation of rotorcraft hub and shaft fairing drag reduction

5. StroubR.YoungL.GrahamD.LouieA. “Investigation of Generic Hub Fairing and Pylon Shapes to Reduce Hub Drag,” NASA TM-10008, 1987.

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1. Wind Tunnel Analysis of Helicopter Aerodynamics with Varying Rotor Head Blade Stub Lengths;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2023-09-23

2. Three Rotor Hub Flow Prediction Workshops (2016-2020) What Did We Learn and What's Next?;J AM HELICOPTER SOC;2023

3. Hub Flow Near-Wake Validation Using CREATE^TM-AV Helios and UMD Mercury Framework;Journal of the American Helicopter Society;2023-01-01

4. Three Rotor Hub Flow Prediction Workshops (2016–2020): What Did We Learn and What's Next?;Journal of the American Helicopter Society;2023-01-01

5. Full-Scale Reynolds Number Testing of Rotor Hub Drag and Wake Turbulence;Journal of the American Helicopter Society;2022-10-01

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