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N-227 Unitary 11ft w.t. safety screen in diffuser ARC-1959-A-24604

N-227 Unitary 11ft w.t. safety screen in diffuser ARC-1959-A-24604

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

Project Mercury: M-1 model in the 11ft w.t. with engineer ARC-1959-A-24777

Project Mercury: M-1 model in the 11ft w.t. with engineer ARC-1959-A-2...

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

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Configuration #5) ARC-1972-A72-1341

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Confi...

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

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Configuration 5 with James M. Peterson ARC-1972-AC72-1344

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Conf...

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

Space Shuttle Two Percent Plumes Model in the 11ft W.T. (Test-01) ARC-1974-AC74-3944

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

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

Oblique wing in 11ft. wind tunnel with R. T. Jones.  Test 11-026. ARC-1975-AC75-0261-33

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

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

Oblique wing in 11ft. wind tunnel with R. T. Jones.  Test 11-026. ARC-1975-AC75-0261-27

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

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

Oblique wing in 11ft. wind tunnel  Test 11-026. ARC-1975-AC75-0261-29

Oblique wing in 11ft. wind tunnel Test 11-026. ARC-1975-AC75-0261-29

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

Oblique wing in 11ft. wind tunnel with R. T. Jones.  Test-11-026. ARC-1975-AC75-0261-8

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

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

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. ARC-1975-AC75-0261-1

Oblique Wing model mounted in 11ft W. T. with R. T. Jones, Designer/En...

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.

Practical Oblique Wing Test-026) in 11ft w.t. overhead view with technician ARC-1975-AC75-0451

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

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

Practical Oblique Wing Test-026) in 11ft w.t.  with R. T. Jones and test engineer ARC-1975-AC75-0450

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

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

CMAPS: 11ft W.T. Test-514 ARC-1983-AC83-0380-4
CMAPS: 11ft W.T. Test-514 ARC-1983-AC83-0380-3
B-1B Shock Induced Ocillation 11x11ft w.t. test-537 ARC-1983-AC83-0667-4

B-1B Shock Induced Ocillation 11x11ft w.t. test-537 ARC-1983-AC83-0667...

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

B-1B Shock Induced Ocillation 11x11ft w.t. test-537 ARC-1983-AC83-0667-5

B-1B Shock Induced Ocillation 11x11ft w.t. test-537 ARC-1983-AC83-0667...

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

Boeing 767 NTF correlation test-611 11ft. w.t. ARC-1984-AC84-0561-1

Boeing 767 NTF correlation test-611 11ft. w.t. ARC-1984-AC84-0561-1

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

Boeing high Reynolds Number Wing Model; 11ft w.t. test-85-1-11 (test-85) ARC-1987-AC87-0783-2

Boeing high Reynolds Number Wing Model; 11ft w.t. test-85-1-11 (test-8...

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

General Dynamics E-7 Full-scale STOVL fighter model fabrication at Ames Model Shop ARC-1987-AC87-0372-143

General Dynamics E-7 Full-scale STOVL fighter model fabrication at Ame...

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

MD-90 Model in NASA Ames Research Center 11ft. Transonic Wind Tunnel  part of the Unitary Plan Wind Tunnel Complex Test-091-1-11 ARC-1990-AC90-0481-8

MD-90 Model in NASA Ames Research Center 11ft. Transonic Wind Tunnel ...

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

Boeing 777 Model 11ft W.T. Test-168 rear view ARC-1969-AC91-0470-3

Boeing 777 Model 11ft W.T. Test-168 rear view ARC-1969-AC91-0470-3

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

Boeing 777 Model 11ft W.T. Test-168 with Wind Tunnel technician Danny Ompoc ARC-1969-AC91-0470-2

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

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

Boeing 777 Model 11ft W.T. Test-168 front view ARC-1991-AC91-0470-1

Boeing 777 Model 11ft W.T. Test-168 front view ARC-1991-AC91-0470-1

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

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11). ARC-1994-AC94-0001-3

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11). ARC-1994-AC94...

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

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11). ARC-1994-AC94-0001-4

Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11). ARC-1994-AC94...

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

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (February and March) ARC-1994-AC94-0134-3

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

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) ARC-1994-AC94-0134-2

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

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) ARC-1994-AC94-0134-8

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

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) ARC-1994-AC94-0134-4

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

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) ARC-1994-AC94-0134-7

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

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) ARC-1994-AC94-0134-6

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

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) ARC-1994-AC94-0134-9

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

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) ARC-1994-AC94-0134-5

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

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 (Wind Tunnel Test Crew) Joe Haudrich, Greg Krakeler, Tom Ccatee, Ron Hathaway, Bud Lanig, Hung Nguyen ARC-1994-AC94-0134-20

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 (Wind Tunnel Test Crew) Jo...

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

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11, 8% Model ARC-1994-AC94-0134-17

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11, 8% Model ARC-1994-AC94-01...

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

F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 ARC-1994-AC94-0134-18
F/A-18 E/F Model: 11ft. W.T. Test #207-1-11 ARC-1994-AC94-0134-19
General Dynamics APKWS rocket test in 11ft w.t. test-11-0122 ARC-2002-ACD04-0007-001

General Dynamics APKWS rocket test in 11ft w.t. test-11-0122 ARC-2002-...

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

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 ARC-2002-ACD02-0101-004

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t....

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 with Doug Atler ARC-2002-ACD02-0101-002

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t....

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 ARC-2002-ACD02-0101-003

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t....

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 ARC-2002-ACD02-0101-001

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t....

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 ARC-2002-ACD02-0101-005

C-5 Re-engineering and Realiability Program semi-span model; 11ft w.t....

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-16 POD test with IR Sensor; 11ft w.t. test-11-0113) with Doug Atler ARC-2003-ACD02-0254-003

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

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

General Dynamics APKWS rocket; 11ft w.t. test-11-0122 ARC-2004-ACD04-0007-003

General Dynamics APKWS rocket; 11ft w.t. test-11-0122 ARC-2004-ACD04-0...

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

General Dynamics APKWS rocket; 11ft w.t. test-11-0122 ARC-2004-ACD04-0007-002

General Dynamics APKWS rocket; 11ft w.t. test-11-0122 ARC-2004-ACD04-0...

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

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel ARC-2006-ACD06-0036-031

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

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. Shown here with Bruce Stroms (l) and James Bell (r) preparing model for test, Danny Ompac and Bill Moede also shown ARC-2006-ACD06-0036-009

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

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

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 ARC-2006-ACD06-0036-016

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

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 ARC-2006-ACD06-0036-014

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

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. Shown here with Bruce Stroms (l) and James Bell (r). ARC-2006-ACD06-0036-008

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

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. Dave Maurantonio  with blue LEDS. ARC-2006-ACD06-0036-040

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

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

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel ARC-2006-ACD06-0036-036

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

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. Joe Olejniczak with blue LEDS. ARC-2006-ACD06-0036-024

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

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

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel ARC-2006-ACD06-0036-034

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

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. Shown here with Danny Ompoc (l), Bruce Stroms (m) and James Bell (r). ARC-2006-ACD06-0036-007

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

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).

CLV (Crew Launch Vehicle) model test in the 11x11ft. W.T. Test-11-0152 with Steve Bucholz ARC-2006-ACD06-0029-005

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

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

CLV (Crew Launch Vehicle) model test in the 11x11ft. W.T. Test-11-0152 ARC-2006-ACD06-0029-002

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

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

CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel. ARC-2006-ACD06-0036-041

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

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

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp ARC-2006-ACD06-0051-015

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

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 ARC-2006-ACD06-0051-002

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

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 ARC-2006-ACD06-0051-012

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

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

3% Space Shuttle Acoustics model test-11-150 in NASA Ames 11x11_foot. Transonic Wind Tunnel on PAL Ramp with Tim Steiger. ARC-2006-ACD06-0051-016

3% Space Shuttle Acoustics model test-11-150 in NASA Ames 11x11_foot. ...

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

3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp ARC-2006-ACD06-0051-018

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

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 ARC-2006-ACD06-0051-007

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

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 ARC-2006-ACD06-0051-009

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

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 ARC-2006-ACD06-0051-008

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

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

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 ARC-2006-ACD06-0052-003

The media invited to view the 3% Space Shuttle model mounted in the Am...

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

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172 ARC-2007-ACD07-0171-004

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) confi...

CEV (Crew Escape Vehicle) Alternative 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 ARC-2007-ACD07-0171-015

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) confi...

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

CEV (Crew Escape Vehicle) Alternaive Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172 ARC-2007-ACD07-0171-016

CEV (Crew Escape Vehicle) Alternaive Launch Abort System (ALAS) config...

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 ARC-2007-ACD07-0171-018

CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) confi...

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

CLV ascent model test 11-0179 11ft. supersonic wind tunnel  with Amela Zanacic removal of model ARC-2008-ACD08-0095-009

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

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

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) ARC-2008-ACD08-0108-001

Next-Generation Aircraft, Pratt and Whitney Ultra-High Bypass Integrat...

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 Boein... more

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel  Test-11-0191 with Amela Zanacic, of Ames/Jacobs Technology ARC-2008-ACD08-0187-003

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ame...

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

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel  Test-11-0191 ARC-2008-ACD08-0187-002

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ame...

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

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. ARC-2008-ACD08-0187-001

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ame...

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.

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel  Test-11-0191 ARC-2008-ACD08-0187-005

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ame...

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

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ames 11ft wind tunnel  Test-11-0191 ARC-2008-ACD08-0187-004

Versatile Affordable Advanced Turbine Engine (VAATE) tested in the Ame...

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

CEV/LAS (Crew Escape Vehicle - Launch Abort System) 51 aeroacoustics test-11-0185 in the Ames Research Center 11ft Transonic Wind Tunnel. ARC-2008-ACD08-0244-003

CEV/LAS (Crew Escape Vehicle - Launch Abort System) 51 aeroacoustics t...

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

2.8% Scale Ares I acoustic model re-entry model in Ames 11ft. Supersonic Wind Tunnel test-11-0192 ARC-2008-ACD08-0266-024

2.8% Scale Ares I acoustic model re-entry model in Ames 11ft. Superson...

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

Space Shuttle 3% acoustics model with Pal ramp in Ames 11ft. w.t. ARC-2009-ACD06-0051-010

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

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

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) ARC-2010-ACD10-0063-013

Common Research Model (CRM) Test t11-0216 in the NASA Ames 11x11_foot ...

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)