Experimental Investigations to Fully Map The Flow Field Around A Wind Tunnel Model of A Transport Airplane

800630

04/01/1980

Authors
Abstract
Content
A description of the results of research conducted to fully map the three-dimensional flow field associated with a typical transport airplane. Details of the method employed to map the flow field, pictures of the longitudinal development of fore body vortices, and a comparison of the experimental results with empirical methods are presented. The results also include a graphic description of the wake propagation behind deflected spoiler panels.
Meta TagsDetails
DOI
https://doi.org/10.4271/800630
Pages
10
Citation
Stremel, P., "Experimental Investigations to Fully Map The Flow Field Around A Wind Tunnel Model of A Transport Airplane," SAE Technical Paper 800630, 1980, https://doi.org/10.4271/800630.
Additional Details
Publisher
Published
Apr 1, 1980
Product Code
800630
Content Type
Technical Paper
Language
English