Swept Wing-Tip Shapes for Low-Speed Airplanes Vigyan Research Associates, Incorporated, Hampton, VA

Format:

Conference/Event

Author/Creator:

van Dam, C. P., author.

Conference Name:

Aerospace Technology Conference & Exposition (1985-10-14 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1985

Summary:

Preliminary results are presented of a study conducted to analyze the effects of several planform modifications on the aerodynamic characteristics of a high-aspect-ratio, natural laminar flow (NLF) wing. The study addresses the potential aerodynamic improvements available at both cruise and high angles of attack by use of swept wing-tip shapes. The swept wing tip appears to offer a viable addition to the lift of wing-tip designs which provide improvements in aerodynamic efficiency, with the added safety benefit of providing high angle-of-attack departure resistance

Notes:

Vendor supplied data

Publisher Number:

851770

Access Restriction:

Restricted for use by site license