Lockheed-Georgia Low Speed Wind Tunnel — Some Implication to Automotive Aerodynamics

690188

2/1/1969

Authors
Abstract
Content
A brief description of the Lockheed-Georgia Co.’s low speed wind tunnel includes discussions of facility characteristics, such as the test section sizes, speed ranges, read-out system capability, balance system limits, and instrumentation hookup capability and versatility. Accessory equipment is also described as it can support wind tunnel testing of automotive vehicles.
Meta TagsDetails
DOI
https://doi.org/10.4271/690188
Citation
Cummings, J., "Lockheed-Georgia Low Speed Wind Tunnel — Some Implication to Automotive Aerodynamics," 1969 International Automotive Engineering Congress and Exposition, Detroit, Michigan, United States, January 13, 1969, https://doi.org/10.4271/690188.
Additional Details
Publisher
Published
2/1/1969
Product Code
690188
Content Type
Technical Paper
Language
English