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DIGITAL LIBRARY: CAMX 2019 | ANAHEIM, CA | SEPTEMBER 23-26

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Allowable Generation and Generic Basis Value for Multiple Loading and Environmental Conditions

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Title: Allowable Generation and Generic Basis Value for Multiple Loading and Environmental Conditions

Authors: Reza Hajiha, Cody Godines, Angelo De Fenza, Harsh Baid, Elizabeth Clarkson, Nima Moazami, and Frank Abdi

DOI: 10.33599/nasampe/c.19.0794

Abstract: Engineers conduct expensive testing in different environmental conditions to obtain the necessary material allowables. These values consider scatter in composite material constituents and structure according to the “Building Block Testing Approach”. There is a need of a robust methodology that can be implemented to predict material properties from Room Temperature to Elevated Temperatures including presence of moisture as well as determine A- and B- basis allowables with reduced testing. The objective is to reduce tests and risk associated with the use of composites in aerospace structures. In this paper a robust methodology is implemented to predict and validate mechanical properties of IM7-8552 material system at various environmental conditions. The proposed methodology will be also used to generate A-basis and B- Basis allowables with limited test data. A multifactor based mathematical model is implemented to calculate mechanical properties at different environmental conditions. The proposed methodology also uses multi-scale progressive failure integrated with probabilistic and statistical approach that consists of: a) Constituent Variation Method (CVM) and Bayesian statistics; and b) Generic Basis strength values for polymer composites to generate allowables with available limited test data. Mechanical properties of IM7-8552 were predicted and validated with NIAR test data for different environmental conditions. Next, cumulative distribution functions, probabilistic sensitivities, and A- and B- Basis Allowables for unidirectional in tension and compression for un-notched composite were validated with physical testing for HEXCEL 8552 IM7 tape in Cold Temperature Dry and Elevated Temperature Wet. The fiber and the matrix properties were calibrated using deterministic Cold Temperature Dry and Elevated Temperature Wet condition strength and stiffnesses. The constituents’ coefficients of variation were initially set to 5% and the software computed real values that likely existed in the test conditions using sensitivities. All simulations were within an acceptable amount of error (less than 2%) for longitudinal tensile, transverse tension and compression and shear loading. Finally, the generic acceptance and equivalence areas for multiple loading and environment conditions were computed and plotted.

References: 1. Frank, Abdi, Elizabeth Clarkson, Cody Godines, Saber DorMohammadi and Angelo De Fenza. "AB Basis Allowable Test Reduction Approach and Composite Generic Basis Strength Values." In 18th AIAA Non-Deterministic Approaches Conference, p. 0951. 2016. 2. Beckwith, Scott W. "Determining Material Properties for Design: Building Block Testing vs. Virtual Testing." (2014): 5-5. 3. The Composite Materials Handbook CMH-17, http://www.cmh17.org/ [Normalization, Test Procedures, Building Block, AB Basis] 4. Hexcel 8552 IM7 Unidirectional Prepreg 190 gsm & 35% RC Qualification Statistical Analysis Report. FAA Special Project Number SP4614WI-Q; NIAR Document NCP-PR-2009-028 Rev A. Report Date: November 16 2012, 2011, Prepared by Elizabeth Clarkson (Ph.D). [NIAR Test Data Allowables] 5. Hexcel 8552 IM7 Unidirectional Prepreg 190 gsm & 35% RC Qualification Material property Data Report. FAA Special Project Number SP4614WI-Q; NCAMP Test Report Number: CAM-PR-2009-015 Rev A. April 22, 2011, Prepared by Kristin Marlett. [NIAR Test Data] 6. Godines, Cody, Saber DorMohammadi, Frank Abdi, Marc Villa Montero, Dade Huang, and Levon Minnetyan. "Damage tolerant composite design principles for aircraft components under static service loading using multi-scale progressive failure analysis." Journal of Composite Materials 51, no. 10 (2017): 1393-1419. 7. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems: Updated Procedure. DOT/FAA/AR03/19, Office of Aviation Research, Washington, D.C. 20591, September 2003. [AB Basis Statistics, Repeatability] 8. G. Abumeri, F. Abdi, K.S. Raju, J. Housner, R. Bohner and A. McCloskey, “Cost Effective Computational Approach for Generation of Polymeric Composite Material Allowables for Reduced Testing”. Book Chapter ISBN 978-953-7619-X-X published by INTECH, Feb-2011. 9. Moazami, Nima & Baid, Harsh & DorMohammadi, Saber & Abdi, Frank & Godines, Cody. (2018). Prediction and Validation of Thermal Mechanical Properties of 3D Printed ULTEM 1010. 10. Browing, C. E., Husman, . E., hitney J. ., “ moisture effects in epoxy matrix composites”, Composite Materials: Testing and Design (4th Conference), ASTM STP 617, pp. 481-496, 1977, Philadelphia, PA 11. Chamis C. C., “Simplified Composite Micromechanics Equations for Hygral, Thermal and Mechanical roperties”, J.W. Weeton et al. (eds), Engineer’s Guide to Composite Materials, 3-8-3-24, ASM International, 1987, Materials Park, OH 12. Chamis, C. C., Sinclair J. H., “Durability/life of fiber composites in hygrothermomechanical environments”, I.M. Daniel (ed.), Composite materials Testing and Design (6th Conference), ASTM STP 787,pp. 498-512, 1982, Philadelphia, PA 13. Villa Montero, Marc, Cody Godines, Frank Abdi, and Levon Minnetyan. "Failure Envelope Validation of Composite Laminates and Environmental Effect." SAMPE 2016, May 23, 2016.

Conference: CAMX 2019

Publication Date: 2019/09/23

SKU: TP19-0794

Pages: 14

Price: $28.00

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