A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2017; you can also visit the original URL.
The file type is application/pdf
.
Comparison of Morphing Wing Stategies Based upon Aircraft Performance Impacts
2004
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference
unpublished
Conventional aircraft are designed for a specific mission and/or set of performance requirements. These requirements often cause the performance for certain mission segments to be compromised because of fixed wing geometry. While some devices, such as flaps, have been used to augment the wing geometry, new materials are being developed that could allow significant wing morphing capability. This paper demonstrates the impact of a morphing wing on aircraft performance and provides a method to
doi:10.2514/6.2004-1722
fatcat:eqfnbxq7irh2lcikqyrs47uiny