The New Chrysler Wind Tunnel

730239

02/01/1973

Event
1973 International Automotive Engineering Congress and Exposition
Authors Abstract
Content
The Chrysler wind tunnel is a closed-circuit, single-return, semiopen jet facility used for performing engine cooling, transmission cooling, engine compartment airflow, underhood component temperature, air-conditioning, and other types of tests. It operates over a 0-120 mph speed range with 400 hp rear-wheel power absorption capacity. Special provisions have been made for idle, city traffic, and tail wind tests. Facility controls provide precise set-point capability, and comprehensive instrumentation and data acquisition systems permit measurement of many parameters and real time data reduction.
Meta TagsDetails
DOI
https://doi.org/10.4271/730239
Pages
8
Citation
Lindsay, J., and Lanktree, H., "The New Chrysler Wind Tunnel," SAE Technical Paper 730239, 1973, https://doi.org/10.4271/730239.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730239
Content Type
Technical Paper
Language
English