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The NCSU Low Speed Boundary Layer Wind Tunnel North Carolina State Univ

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Nagel, R. T., author.
Conference Name:
Aerospace Technology Conference & Exposition (1985-10-14 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1985
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
851897
Access Restriction:
Restricted for use by site license

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