Deflection-Based Aircraft Structural Loads Estimation With Comparison To Flight-Reference-Cited by-同舟云学术

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Deflection-Based Aircraft Structural Loads Estimation With Comparison To Flight

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
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Author:

Lizotte Andrew¹,Lokos William¹

Affiliation:

1. NASA Dryden Flight Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2016

Reference17 articles.

1. 1Skopinski, T.H., Aiken, W.S., and Huston, W.B. "Calibration of Strain-Gage Installations in Aircraft Structures for the Measurement of Flight Loads," NACA Report 1178, 1954.

2. Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development

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