Publication Date:
2019-07-13
Description:
NASA Glenn Research Center and Lockheed Martin tested an aircraft model in two wind tunnels to compare low-speed (subsonic) flow characteristics. Test objectives were to determine and document similarities and uniqueness of the tunnels and to verify that the 10- by 10-Foot Supersonic Wind Tunnel (10x10 SWT) is a viable low-speed test facility when compared to the 8- by 6-Foot Supersonic Wind Tunnel (8x6 SWT). Conclusions are that the data from the two facilities compares very favorably and that the 10-by 10-Foot Supersonic Wind Tunnel at NASA Glenn Research Center is a viable low-speed wind tunnel.
Keywords:
Aerodynamics
Type:
NASA/TM-2002-211516
,
NAS 1.15:211516
,
E-13309
,
22nd Aerodynamic Measurement Technology and Ground Testing Conference; Jun 24, 2002 - Jun 26, 2002; St. Louis, MO; United States
Format:
application/pdf
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