Normal stress flow evaluation in composite aircraft wing sections by Strength of Material models

Composite Structures ◽

10.1016/j.compstruct.2021.115088 ◽

2021 ◽

pp. 115088

Author(s):

J.C. Marín ◽

E. Graciani

Keyword(s):

Normal Stress ◽

Aircraft Wing ◽

Material Models ◽

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On the Validity of the Maxwell Model and Related Constitutive Equations; a Study Based on the First Normal Stress Coefficient

Journal de Physique I ◽

10.1051/jp1:1997153 ◽

1997 ◽

Vol 7 (12) ◽

pp. 1523-1533

Author(s):

H.-P. Wittmann

Keyword(s):

Normal Stress ◽

Constitutive Equations ◽

Maxwell Model ◽

Stress Coefficient

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Closed-form Solutions for Predicting Interlaminar Shear Stress and Hygrothermomechanical Normal Stress in Composite Beams with Rectangular and Tubular Cross-sections

10.33599/nasampe/s.19.1364 ◽

2019 ◽

Author(s):

Sthanu Mahadev ◽

Wen Chan ◽

Reiley Schraeger

Keyword(s):

Shear Stress ◽

Closed Form ◽

Normal Stress ◽

Cross Sections ◽

Composite Beams ◽

Closed Form Solutions ◽

Interlaminar Shear Stress ◽

Interlaminar Shear

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Analysis of Drag for an Aircraft Wing Model with and without Winglet

Indian Journal Of Applied Research ◽

10.15373/2249555x/apr2012/27 ◽

2011 ◽

Vol 1 (7) ◽

pp. 89-91

Author(s):

Mitul Patel ◽

◽

Sharvil Shah ◽

Dharmendra Dubey

Keyword(s):

Aircraft Wing ◽

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ABOUT METHODS OF DETEMINING BUFFET ONSET BOUNDARY FOR A PASSENGER AIRCRAFT WING

TsAGI Science Journal ◽

10.1615/tsagiscij.2018029594 ◽

2018 ◽

Vol 49 (8) ◽

pp. 809-823

Author(s):

Nikolay Nikolaevich Bragin

Keyword(s):

Aircraft Wing ◽

Passenger Aircraft

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Construction of Compressible Euler Solver Using Building-Cube Method and Application to Flutter Analysis of Aircraft Wing

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ◽

10.2322/jjsass.62.39 ◽

2014 ◽

Vol 62 (2) ◽

pp. 39-46 ◽

Author(s):

Yasutaka NISHIMURA ◽

Daisuke SASAKI ◽

Kazuhiro NAKAHASHI

Keyword(s):

Aircraft Wing ◽

Flutter Analysis ◽

Compressible Euler ◽

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Abhangigkeit der Normalspannungsdifferenz von der Schubspannung / Relationship between the Normal Stress Difference and the Shear Stress

Applied Rheology ◽

10.2478/arh-1995-050108 ◽

1995 ◽

Vol 5 (1) ◽

pp. 29-33 ◽

Author(s):

Dimiter Hadjistamov

Keyword(s):

Shear Stress ◽

Normal Stress ◽

Normal Stress Difference ◽

Stress Difference

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Coupled thermoelasticity of shells of revolution - Effect of normal stress and coupling

AIAA Journal ◽

10.2514/3.14197 ◽

1999 ◽

Vol 37 ◽

pp. 496-504

Author(s):

M. R. Eslami ◽

M. Shakeri ◽

A. R. Ohadi ◽

B. Shiari

Keyword(s):

Normal Stress ◽

Shells Of Revolution ◽

Coupled Thermoelasticity

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Identification of the static and dynamic numerical model of a jet aircraft wing from experimental tests

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-1498 ◽

2021 ◽

Author(s):

Claudio Chiodi ◽

Giuliano Coppotelli ◽

Jacopo Valentino Covioli

Keyword(s):

Numerical Model ◽

Experimental Tests ◽

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Challenges Towards Developing a High Fidelity Database for Validating High Strain Rate Composite Material Models

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-1404 ◽

2021 ◽

Author(s):

Mark Pankow ◽

Joseph Giliberto ◽

Brandon Hearley ◽

Brian Justusson ◽

Joseph Schaefer ◽

...

Keyword(s):

Composite Material ◽

High Strain Rate ◽

Strain Rate ◽

High Strain ◽

High Fidelity ◽

Material Models

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Nondestructive Evaluation (NDE) Technology Initiatives (NTIP). Delivery Order 0039: Statistical Comparison of Competing Material Models

10.21236/ada415275 ◽

2003 ◽

Author(s):

Charles Annis

Keyword(s):

Nondestructive Evaluation ◽

Material Models ◽

Statistical Comparison ◽

Technology Initiatives

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