Aerodynamic Tailoring of the Learjet Model 60 Wing Learjet Incorporated

Format:

Conference/Event

Author/Creator:

Chandrasekharan, Reuben M., author.

Conference Name:

Aerospace Technology Conference & Exposition (1993-09-20 : Anaheim, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1993

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

932534

Access Restriction:

Restricted for use by site license