Aerodynamic Tailoring of the Learjet Model 60 Wing

Paper #:
  • 932534

Published:
  • 1993-09-01
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.
Pages:
9
Abstract:
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.
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