Some Recent Innovations in Wind Tunnel Testing Techniques

690677

02/01/1969

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
In recent years, several innovations have been made in wind tunnel testing techniques which have significantly improved the testing cost effectiveness. Use of colored water spray in low speed testing causes unsuspected vortices to stand out allowing quick and accurate drag reduction filleting to be prepared. Simultaneous force and pressure model transonic testing has reduced the time and cost to arrive at a low drag airplane configuration by more than 50%. Means are being developed to accurately predict high Reynolds number transonic airloads from low Reynolds number data. The use of accurately sized glass beads to provide boundary layer transition for transonic testing has been found to reduce run-to-run drag data scatter by more than 50%.
Meta TagsDetails
DOI
https://doi.org/10.4271/690677
Pages
8
Citation
Wilson, F., and Maddox, B., "Some Recent Innovations in Wind Tunnel Testing Techniques," SAE Technical Paper 690677, 1969, https://doi.org/10.4271/690677.
Additional Details
Publisher
Published
Feb 1, 1969
Product Code
690677
Content Type
Technical Paper
Language
English