The NCSU Low Speed Boundary Layer Wind Tunnel

851897

10/01/1985

Authors
Abstract
Content
Procedures employed for the design of a new low speed boundary layer wind tunnel are described. The tunnel is a semi-open circuit facility for the study of large scale two-dimensional boundary layers with or without pressure gradients, A large plenum box is used as a replacement for a diffuser, 90 degree turn and noise attenuation chamber. The modular test section is seven meters long and capable of velocities from 5 to 33 m/sec. Experimental data to evaluate the tunnel performance are also described.
Meta TagsDetails
DOI
https://doi.org/10.4271/851897
Pages
12
Citation
Nagel, R., and Alaverdi, O., "The NCSU Low Speed Boundary Layer Wind Tunnel," SAE Technical Paper 851897, 1985, https://doi.org/10.4271/851897.
Additional Details
Publisher
Published
Oct 1, 1985
Product Code
851897
Content Type
Technical Paper
Language
English