Synthesis of In-Flight Strains Using Flight Parameters for a Fighter Aircraft-Reference-Cited by-同舟云学术

Synthesis of In-Flight Strains Using Flight Parameters for a Fighter Aircraft

Published:2013-03 Issue:2 Volume:50 Page:469-477
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sharan Agam¹,Vijayaraju K.¹,James Deepa¹

Affiliation:

1. Aeronautical Development Agency, Bangalore 560017, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031888

Reference24 articles.

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2. DoreS.GinsburgD. “A-3 Strain-Measured Fatigue Tracking,” Aerostructures Inc. TR88015, Arlington, VA, 1988.

3. SchützW. “Fatigue Life Prediction for Aircraft Structures and Materials,” AGARD LS-62, ICAF-Doc-693, Neuilly-sur-Seine, France, 1973.

4. Identification of helicopter component loads using multiple regression

5. AzzamH. “The Use of Helicopter Flight Parameters for Fatigue Damage Prediction,” Smiths Aerospace, Electronic Systems, Rept. MJAD/R/125/93v1.0, Southampton, April 1993.

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