Structural Design Synthesis of Aircraft Engine Pylons at Certification Level of Detail
Author:
Affiliation:
1. University of Washington, Seattle, WA 98195
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035953
Reference26 articles.
1. WanhillR. J. H.OldersmaA. “Fatigue and Fracture in an Aircraft Engine Pylon,” National Aerospace Lab., NLR TP 96719, 1997, https://core.ac.uk/download/pdf/80112240.pdf.
2. ATSB Transport Safety Report, “Engine Pylon Carcking Involving Boeing 747-438, VH-OJT,” Australian Transport Safety Bureau, AO-2016-148, June 2016.
3. Development of a Load Sensor for Aircraft Pylon Interface Load Measurement
4. Investigation About the Structural Nonlinearities of an Aircraft Pylon
5. CazierF. Jr.KehoeM. “Flight Test of a Decoupler Pylon for Wing/Store Flutter Suppression,” AIAA Paper 1986-9730, 1986. 10.2514/6.1986-9730
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