Aerodynamic Impacts of Helicopter Blade Erosion Coatings-Reference-Cited by-同舟云学术

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Aerodynamic Impacts of Helicopter Blade Erosion Coatings

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Calvert Mark¹,Wong Tin-chee¹

Affiliation:

1. Army Research, Development and Engineering Command

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2914

Reference14 articles.

1. 1Ward,K.E."TheEffectofSmallVariationsinProfileofAirfoils,"NACATN361,1931.

2. 2Jacobs,E.N."AirfoilSectionCharacteristicsasAffectedbyProtuberances,"NACATR446,1934.

3. 3Jacobs,E.N.,andSherman,A."WingCharacteristicsasAffectedbyProtuberancesofShortSpan,"NACATR449,1934.

4. 4Cebici,T."EffectsofEnvironmentallyImposedRoughnessonAirfoilPerformance,"NASACR-179639,1987.

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1. Evaluation of a Serrated Edge to Mitigate the Adverse Effects of a Backward-Facing Step on an Airfoil;Inventions;2023-12-18

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3. Investigation of Wake Survey over a Wing with Conformal Vortex Generators;AIAA Scitech 2019 Forum;2019-01-06

4. A multiple particle impact model for prediction of erosion in carbon-fiber reinforced composites;Wear;2018-07

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