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Dive into the research topics where David B. Curliss is active.

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Featured researches published by David B. Curliss.


Journal of Polymer Science Part B | 1997

Isochoric and isobaric glass formation : Similarities and differences

Dina M. Colucci; Gregory B. McKenna; James J. Filliben; Andre Lee; David B. Curliss; Keith B. Bowman; John D. Russell

Pressure-volume-temperature (PVT) studies were performed on a glass-forming polymer, poly(carbonate) (PC), under both isobaric and isochoric (constant volume) conditions. An isochoric glass transition was observed and the formation points were found to be consistent with those obtained isobarically. Although the isobaric and isochoric responses were, as expected, the same in the rubbery state, the glassy state values were found to be different and dependent upon the glass formation history. The isobaric data exhibited larger changes in going from the rubber to the glass, hence a stronger glass transition, than did the isochoric data. Inserting the experimental values for the thermal expansion coefficient α and isothermal compressibility β, into appropriate thermodynamic relations, measures of the strength of each transition are defined. Strength estimates based on literature values of α and β are compared to the experimental measures of the isochoric and isobaric transitions. In addition, both the isobaric and isochoric PVT results were analyzed in terms of the Fox and Flory free volume theory which assumes that the glass transition is an iso-free volume state. While the isobaric results were consistent with the Fox and Flory theory, the isochoric results were not consistent with the idea of an iso-free volume glass transition.


Journal of Thermoplastic Composite Materials | 1992

Effects of Thermal History and Jet Fuel Absorption on the Properties of APC-2

John D. Russell; David B. Curliss

The response of APC-2 (AS4/PEEK) processed with different thermal histories simulating different fabrication techniques was investigated. Three thermal histories were evaluated: (1) slow cooled (SC) from the melt state at 2°C/min; (2) rapidly quenched (Q) from the melt state by cold press transfer; and (3) quenched and annealed (Q/A) at 160°C. The SC APC-2 was found to have a fully developed semicrystalline matrix and the highest strength and modulus for flexural and shear tests, while the Q APC- 2 was found to have an essentially amorphous matrix and the greatest fracture toughness. In uniaxial creep tests of [±45°]2 S coupons both exposed and unexposed to JP-4, the unexposed Q specimens had the highest creep rates at room temperature and 100°C. The exposed SC specimens had the highest creep rates at 100°C because of the plasticization effect of the absorbed JP-4.


Archive | 2008

Vapor grown carbon fiber reinforced composite materials and methods of making and using same

David B. Curliss; Jason E. Lincoln


Journal of Applied Polymer Science | 2003

PREPARATION, CHARACTERIZATION AND NANOSTRUCTURAL EVOLUTION OF EPOXY NANOCOMPOSITES

Chenggang Chen; David B. Curliss


Archive | 2008

Continuous process for the production of carbon nanofiber reinforced continuous fiber preforms and composites made therefrom

David B. Curliss; Jason E. Lincoln


Journal of Thermoplastic Composite Materials | 2000

Hygrothermal Durability and Thermal Aging Behavior Prediction of High-Temperature Polymer-Matrix Composites and Their Resins

E. Eugene Shin; Roger J. Morgan; Jiming Zhou; Jason E. Lincoln; Robert Jurek; David B. Curliss


Archive | 2004

Processable thermally stable addition polyimide for composite applications

David B. Curliss; Jason E. Lincoln; Katie E. Thorp


Polymer Composites | 2008

Effect of matrix chemical structure on the thermo-oxidative stability of addition cure poly(imide siloxane) composites

Jason E. Lincoln; Roger J. Morgan; David B. Curliss


Journal of Applied Polymer Science | 2008

High temperature organic/inorganic addition cure polyimide composites, part 1: Matrix thermal properties

Jason E. Lincoln; Sara Hout; Kelly Flaherty; David B. Curliss; Roger J. Morgan


Archive | 2016

FIBER WINDING SYSTEM FOR COMPOSITE PROJECTILE BARREL STRUCTURE

Jason E. Lincoln; David B. Curliss

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Jason E. Lincoln

Air Force Research Laboratory

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John D. Russell

Wright-Patterson Air Force Base

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Robert Jurek

Michigan State University

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Chenggang Chen

University of Dayton Research Institute

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Dina M. Colucci

National Institute of Standards and Technology

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Andre Lee

Michigan State University

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Brian Rook

Michigan State University

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E. Eugene Shin

Michigan State University

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