Aerodynamic Tailoring of the Learjet Model 60 Wing

932534

09/01/1993

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
The wing of the Learjet Model 60 was tailored for improved aerodynamic characteristics using the TRANAIR transonic full-potential CFD code. A root leading edge glove and wing tip fairing were shaped to reduce shock strength, improve cruise drag and extend the buffet limit. The aerodynamic design was validated by wind tunnel test and flight test data.
Meta TagsDetails
DOI
https://doi.org/10.4271/932534
Pages
9
Citation
Chandrasekharan, R., Hawke, V., Hinson, M., Kennelly, R. et al., "Aerodynamic Tailoring of the Learjet Model 60 Wing," SAE Technical Paper 932534, 1993, https://doi.org/10.4271/932534.
Additional Details
Publisher
Published
Sep 1, 1993
Product Code
932534
Content Type
Technical Paper
Language
English