Flow Field Around Thick Delta Wing with Rounded Leading Edge

912009

09/01/1991

Event
International Pacific Air & Space Technolgy Conference
Authors Abstract
Content
A thick delta wing with a rounded leading egde has been experimentally studied. To understand the basic flow field of such a wing, experiments have been conducted in low speed wind tunnel at Nagoya university. Three types of flow visualization: oil flow, smoke wire, and tuft methods are employed, and forces: lift and drag, and pressure distributions were also obtained. The same test has been conducted for a thin delta wing for comparison.
The results show the different flow field of the thick delta wing from those commonly known for delta wings. However, in other properties except for the flow pattern, similarities were observed between the thick delta wing and thin delta wing.
Meta TagsDetails
DOI
https://doi.org/10.4271/912009
Pages
12
Citation
Nakajima, Y., Nakao, Y., Nakamura, Y., and Yasuhara, M., "Flow Field Around Thick Delta Wing with Rounded Leading Edge," SAE Technical Paper 912009, 1991, https://doi.org/10.4271/912009.
Additional Details
Publisher
Published
Sep 1, 1991
Product Code
912009
Content Type
Technical Paper
Language
English