Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction

R. Ashworth, S. Lawson, R. Lowry, A. Martinez-Cava, S. Mughal, H. Roland, C. Thomas

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

Original languageEnglish
Title of host publication2016 Applied Aerodynamics Conference
Subtitle of host publicationevolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol
PublisherRoyal Aeronautical Society
Pages336-349
Number of pages14
ISBN (Electronic)9781857683714
Publication statusPublished - 2016
Externally publishedYes

Cite this

Ashworth, R., Lawson, S., Lowry, R., Martinez-Cava, A., Mughal, S., Roland, H., & Thomas, C. (2016). Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. In 2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol (pp. 336-349). Royal Aeronautical Society.