Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing

Butt, Lauren M.; Kurdi, Mohammad; Kapania, Rakesh K.; Asheghian, Laila

doi:10.2514/6.2011-1970

Cited by 3 publications

(1 citation statement)

References 11 publications

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“…Therefore, only Aramid (Kevlar and Technora) and LCP (Vectran) remain as the most suitable material for inflatable wing application and the proof that these material are the best is the fact that many research group on inflatable structure are using either of this material for their research [23,27,[37][38][39][40][41][42].…”

Section: J Fundam Appl Sci 2017 9(3s) 317-334 324mentioning

confidence: 99%

Inflatable structure for aerospace application: Historical perspective and future outlook

Dollah

Saad

CheIdris

2018

J. Fundam and Appl Sci.

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This is an overview topic of inflatable structure for aerospace application. An inflatable structure is a promising choice for a wide r application are inflatable wing, space antenna, solar array, inflatable aeroshell and inflatable aerodynamic decelerators. The advantages of inflatable structure are it offers the potential for compact stowing of lightweight structure. This will efficient packaging, easy to deploy and ultimately lead to reduction in mission cost.Historically, inflatable technology has been introduced as a concept in aerospace application with a patent on flying glider th Over the years, many concepts of inflatable were introduced but only a small number of concepts have progress beyond the stage of design and even fewer manage to be completed and used extensively.

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Section: J Fundam Appl Sci 2017 9(3s) 317-334 324mentioning

confidence: 99%

Inflatable structure for aerospace application: Historical perspective and future outlook

Dollah

Saad

CheIdris

2018

J. Fundam and Appl Sci.

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Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing

Loh¹,

Gaddam²,

Jacob³

et al. 2012

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

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Buckling and Vibrations of Periodically Supported Non-Prismatic Columns using an Integral Equation Approach
Miglani
¹
,
Kapania
²

2020
AIAA Scitech 2020 Forum
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Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing

Cited by 3 publications

References 11 publications

Inflatable structure for aerospace application: Historical perspective and future outlook

Inflatable structure for aerospace application: Historical perspective and future outlook

Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing

Buckling and Vibrations of Periodically Supported Non-Prismatic Columns using an Integral Equation Approach

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