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11-Foot Transonic Unitary Plan Facility
11-Foot Transonic Unitary Plan Facility Home
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Gallery
Fighter model mounted in the 11-Foot Transonic Unitary Plan Facility at ARC Blue-lit image of scale model of Crew Exploration Vehicle (CEV) at NASA Ames Research Center, Moffett Field, Calif., in early March 200
Gallery
ACD06-0036-014: Blue-lit image of scale model of Crew Exploration Vehicle (CEV) at NASA Ames Research Center, Moffett Field, Calif., in early March 2006 ACD06-0036-014
Blue-lit image of scale model of Crew Exploration Vehicle (CEV) at NASA Ames Research Center, Moffett Field, Calif., in early March 2006.
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ACD06-0029-010: Test engineer Steve Buchholz adjusts the Crew Launch Vehicle (CLV) model in the 11-foot wind tunnel at NASA Ames Research Center ACD06-0029-010
Test engineer Steve Buchholz adjusts the Crew Launch Vehicle (CLV) model in the 11-foot wind tunnel at NASA Ames Research Center.
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ACD06-0036-009: Scale model of Crew Exploration Vehicle (CEV), covered in plastic sheeting, is being prepared for testing in the Unitary Wind Tunnel Complex at NASA Ames Research Center, Moffett Field, Calif., in early March 2006 ACD06-0036-009
Scale model of Crew Exploration Vehicle (CEV), covered in plastic sheeting, is being prepared for testing in the Unitary Wind Tunnel Complex at NASA Ames Research Center, Moffett Field, Calif., in early March 2006.
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3% Scale Space Shuttle Aero Acoustics IS-21 Model being tested in the 11-by 11-foot Transonic Wind Tunnel ACD06-0051-010
3% Scale Space Shuttle Aero Acoustics IS-21 Model being tested in the 11-by 11-foot Transonic Wind Tunnel. The purpose of this test was to determine the aero effects on the external tank protuberances with and without the PAL ramps.
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EA-18G Model being tested in the 11-by 11-foot Transonic Wind Tunnel at NASA Ames Research Center ACD04-0177-001
EA-18G Model being tested in the 11-by 11-foot Transonic Wind Tunnel at NASA Ames Research Center. The purpose of this test was to obtain aerodynamic force and moment data.
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AC96-5007-12: N-227 Unitary Plan Wind Tunnel Modification Project (UMP); Diffuser and contraction vanes AC96-5007-12
N-227 Unitary Plan Wind Tunnel Modification Project (UMP); Diffuser and contraction vanes.
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AC80-0459-2: N-227 Unitary Plan Wind Tunnel Modification Project (UMP); Diffuser and contraction vanes AC80-0459-2
VSTOL F-1 (HAVTOL) in 11x11ft w.t. test-252
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Further Information
NASA's ATP Program
Read about one of the largest, most versatile and comprehensive set of testing facilities in the nation.
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11-Foot Transonic Unitary Plan Facility
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NASA Ames Windtunnels
Get further information about the 9'x7' SWT and 11'x11' TWT facilities at NASA Ames.
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Ames Research Center
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NASA - National Aeronautics and Space Administration
NASA Official: Tony Springer
Last Updated: October 17, 2011
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