CMAPS: 11ft W.T. Test-514

CMAPS: 11ft W.T. Test-514

General Dynamics APKWS rocket; 11ft w.t. test-11-0122

General Dynamics APKWS rocket; 11ft w.t. test-11-0122

Oblique wing in 11ft. wind tunnel Test 11-026.

Practical Oblique Wing Test-026) in 11ft w.t. overhead view with technician

General Dynamics APKWS rocket test in 11ft w.t. test-11-0122

Project Mercury: M-1 model in the 11ft w.t. with engineer

N-227 Unitary 11ft w.t. safety screen in diffuser

Oblique wing in 11ft. wind tunnel with R. T. Jones. Test-11-026.

Practical Oblique Wing Test-026) in 11ft w.t. with R. T. Jones and test engineer

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel

Oblique wing in 11ft. wind tunnel with R. T. Jones. Test 11-026.

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel Test-11-0191

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel

CLV ascent model test 11-0179 11ft. supersonic wind tunnel with Amela Zanacic removal of model

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel.

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel Test-11-0191

Oblique wing in 11ft. wind tunnel with R. T. Jones. Test 11-026.

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel Test-11-0191

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel

Space Shuttle 3% acoustics model with Pal ramp in Ames 11ft. w.t.

Boeing 777 Model 11ft W.T. Test-168 front view

Boeing 767 NTF correlation test-611 11ft. w.t.

Boeing 777 Model 11ft W.T. Test-168 rear view

Space Shuttle Two Percent Plumes Model in the 11ft W.T. (Test-01)

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Dave Maurantonio with blue LEDS.

2.8% Scale Ares I acoustic model re-entry model in Ames 11ft. Supersonic Wind Tunnel test-11-0192

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Danny Ompoc preparing for testing.

CEV (Crew Escape Vehicle) Alternaive Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172 with Paul Espinosa

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel Test-11-0191 with Amela Zanacic, of Ames/Jacobs Technology

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Joe Olejniczak with blue LEDS.

CEV/LAS (Crew Escape Vehicle - Launch Abort System) 51 aeroacoustics test-11-0185 in the Ames Research Center 11ft Transonic Wind Tunnel.

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Configuration 5 with James M. Peterson

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Configuration #5)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11, 8% Model

Boeing 777 Model 11ft W.T. Test-168 with Wind Tunnel technician Danny Ompoc

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

Boeing high Reynolds Number Wing Model; 11ft w.t. test-85-1-11 (test-85)

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March)

F-16 POD test with IR Sensor; 11ft w.t. test-11-0113) with Doug Atler

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Shown here with Paul Espinosa (l) and Tuan Truong (r) wwith blue LEDS

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Shown here with Bruce Stroms (l) and James Bell (r).

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Shown here with Danny Ompoc (l), Bruce Stroms (m) and James Bell (r).

MD-90 Model in NASA Ames Research Center 11ft. Transonic Wind Tunnel part of the Unitary Plan Wind Tunnel Complex Test-091-1-11

Oblique Wing model mounted in 11ft W. T. with R. T. Jones, Designer/Engineer. The asymmetrical design allows the plane to fly much faster, yet consume the same fuel and generate less noise.

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel Test-11-0191 with Alex Giese and Jeff Aiello of the Air Force Research Laboratory.

The media invited to view the 3% Space Shuttle model mounted in the Ames 11ft .w.t. with Scott Budman, NBC Channel 11 News and Jim Strong, Ames Aeronautics

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t. Test-11-0103; Throught flow nacelle and inboard nacelle with turbine propulsion systems unit with Doug Atler

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t. Test-11-0103; Throught flow nacelle and inboard nacelle with turbine propulsion systems unit

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t. Test-11-0103; Throught flow nacelle and inboard nacelle with turbine propulsion systems unit

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (Wind Tunnel Test Crew) Joe Haudrich, Greg Krakeler, Tom Ccatee, Ron Hathaway, Bud Lanig, Hung Nguyen

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t. Test-11-0103; Throught flow nacelle and inboard nacelle with turbine propulsion systems unit

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t. Test-11-0103; Throught flow nacelle and inboard nacelle with turbine propulsion systems unit

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. Shown here with Bruce Stroms (l) and James Bell (r) preparing model for test, Danny Ompac and Bill Moede also shown

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp

Next-Generation Aircraft, Pratt and Whitney Ultra-High Bypass Integration test at NASA Ames 11ft. wind tunnel (test 11-0182) assess the interaction effects of a scaled Pratt & Whitney geared turbofan on a Boeing 737-800 fuselage in an effort to use emerging technologies to make next-generation airliners quieter, more fuel efficient and lower on emissions. (printed in Aviation Week & Space Technology April 8, 2011 issue)

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11).

CLV (Crew Launch Vehicle) model test in the 11x11ft. W.T. Test-11-0152

General Dynamics E-7 Full-scale STOVL fighter model fabrication at Ames Model Shop

B-1B Shock Induced Ocillation 11x11ft w.t. test-537

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11).

Common Research Model (CRM) Test t11-0216 in the NASA Ames 11x11_foot Transonic Wind Tunnel with PIV laser sheet over model. (3D PIV Particle Image Velosymetry Equipment)

CLV (Crew Launch Vehicle) model test in the 11x11ft. W.T. Test-11-0152 with Steve Bucholz

B-1B Shock Induced Ocillation 11x11ft w.t. test-537

3% Space Shuttle Acoustics model test-11-150 in NASA Ames 11x11_foot. Transonic Wind Tunnel on PAL Ramp with Tim Steiger.