Strain-Gage Loads Calibration Testing of the Active Aeroelastic Wing F/A-18 Aircraft-Reference-Cited by-同舟云学术

Strain-Gage Loads Calibration Testing of the Active Aeroelastic Wing F/A-18 Aircraft

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
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Author:

Lokos William¹,Olney Candida¹,Chen Tony¹,Crawford Natalie¹,Stauf Rick²,Reichenbach E.³

Affiliation:

1. NASA Dryden Flight Research Center

2. Spiral Technology Inc

3. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2926

Reference11 articles.

1. 2Pendleton, Ed, Kenneth Griffin, Michael W. Kehoe, and Boyd Perry, "A Flight Research Program for Active Aeroelastic Wing Technology," AIAA-96-1574-CP, April1996,pp.2263-2273.

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

3. 4Lokos,WilliamA.,etal."WingTorsionalStiffness Tests of the Active Aeroelastic Wing F/A-18 Airplane," AIAA-2002-1333,Jan.2002.

4. 5Skopinski,T.H.,WilliamS.Aiken,Jr.,andWilberB. Huston, Calibration of Strain-Gage Installations In Aircraft Structures For The Measurement Of Flight Loads,NACAReport1178,1954.

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