Internal Geometry Effects on Inherent Damping Performance of Additively Manufactured Components-Reference-Cited by-同舟云学术

Internal Geometry Effects on Inherent Damping Performance of Additively Manufactured Components

Published:2021-01 Issue:1 Volume:59 Page:379-385
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Scott-Emuakpor Onome¹,Schoening Austin²,Goldin Andrew¹,Beck Joseph¹,Runyon Brian¹,George Tommy¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

2. Universal Technology Corporation, Dayton, OH 45432

Funder

United States Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference34 articles.

1. “Department of Defense Handbook: Engine Structural Integrity Program (ENSIP),” U.S. Dept. of Defense, U.S. Air Force Rept. MIL-HDBK-1783B, Feb. 2002.

2. Blade vibration - Some key elements in design verification

3. An analytical particle damping model

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