Design and Testing of a Blended Wing Body Aeroelastic Wind-Tunnel Model

Carlsson, Martin; Kuttenkeuler, Jakob

doi:10.2514/2.3079

Cited by 7 publications

(1 citation statement)

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“…French [1][2] et al Proposed a design method of elastic model, and used the method of increasing counterweight to make the model meet the dynamic similarity, and completed the corresponding test. Carlson [3] and others designed a model of an aircraft by using the aeroelastic cutting method. The internal beam is used to maintain the stiffness, and the external rigid wing surface is used to maintain the aerodynamic shape.…”

Section: Introductionmentioning

confidence: 99%

Design Technology of Aircraft Full Elastic Model Based on Multiple Materials

Hou

Liu

2022

Advances in Transdisciplinary Engineering

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This paper introduces the design requirements and design methods of structural materials in the process of aircraft model design, and introduces the shortcomings of traditional methods in this kind of structural design. Based on this, a full elastic model design method combining metal and composite materials is established. This method has the characteristics of accurate and fast design and simple structure. In order to verify the effectiveness of this method, this paper lists two related aircraft model structure design schemes, and introduces the design process and design results. The experimental results show that the above method can effectively complete the aircraft full elastic model design, the model design is accurate, and can meet the needs of aircraft simulation.

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Section: Introductionmentioning

confidence: 99%