Experimental validation of tow-steered composite wings for aeroelastic design

O. Stodieck, G. Francois, D. Heathcote, E. Zympeloudis, B. C. Kim, A. T. Rhead, D. Cleaver, J. E. Cooper

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

A numerical and experimental investigation is described considering the design, manufacture and test of tow-steered composite wind tunnel wings. The generic construction of each wing consisted of a rectangular flat plate with foam aerofoil surfaces. Tow-steered composite layers of the wings were manufactured using two different techniques: Continuous Tow-Shearing and Discrete Stiffness Tailoring. Finite Element models of the wings were optimised in order to determine the tow-steered composite layer orientations, as well as unidirectional composite orientations, that reduced the maximum strains due to equivalent “manoeuvre” and “gust” loads (at a tunnel speed of 20 m/s). A series of static and dynamic, wind-on and wind-off tests were performed to validate the numerical modelling capability and to illustrate the capabilities of tow-steering technologies.

Original languageEnglish
Title of host publication17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
PublisherInternational Forum on Aeroelasticity and Structural Dynamics (IFASD)
Volume2017-June
ISBN (Electronic)9788897576280
Publication statusPublished - 1 Jan 2017
Event17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 - Como, Italy
Duration: 25 Jun 201728 Jun 2017

Conference

Conference17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017
CountryItaly
CityComo
Period25/06/1728/06/17

Keywords

  • Aeroelastic optimisation
  • Aeroelastic tailoring
  • Tow-steering

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

Cite this

Stodieck, O., Francois, G., Heathcote, D., Zympeloudis, E., Kim, B. C., Rhead, A. T., ... Cooper, J. E. (2017). Experimental validation of tow-steered composite wings for aeroelastic design. In 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017 (Vol. 2017-June). International Forum on Aeroelasticity and Structural Dynamics (IFASD).

Experimental validation of tow-steered composite wings for aeroelastic design. / Stodieck, O.; Francois, G.; Heathcote, D.; Zympeloudis, E.; Kim, B. C.; Rhead, A. T.; Cleaver, D.; Cooper, J. E.

17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. Vol. 2017-June International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2017.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Stodieck, O, Francois, G, Heathcote, D, Zympeloudis, E, Kim, BC, Rhead, AT, Cleaver, D & Cooper, JE 2017, Experimental validation of tow-steered composite wings for aeroelastic design. in 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. vol. 2017-June, International Forum on Aeroelasticity and Structural Dynamics (IFASD), 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017, Como, Italy, 25/06/17.
Stodieck O, Francois G, Heathcote D, Zympeloudis E, Kim BC, Rhead AT et al. Experimental validation of tow-steered composite wings for aeroelastic design. In 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. Vol. 2017-June. International Forum on Aeroelasticity and Structural Dynamics (IFASD). 2017
Stodieck, O. ; Francois, G. ; Heathcote, D. ; Zympeloudis, E. ; Kim, B. C. ; Rhead, A. T. ; Cleaver, D. ; Cooper, J. E. / Experimental validation of tow-steered composite wings for aeroelastic design. 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017. Vol. 2017-June International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2017.
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