Canard Rotor test 80x120ft. w.t test-80-0024
ARC-1969-AC96-0328-6
Canard Rotor test 80x120ft. w.t test-80-0024
ARC-1969-AC96-0328-3
Canard Rotor test 80x120ft. w.t test-80-0024
ARC-1969-AC96-0328-8
Canard Rotor test 80x120ft. w.t test-80-0024
ARC-1969-AC96-0328-9
Advanced Recovery Systems Parafoil test 80x120ft w.t. test-004
ARC-1988-AC88-0537-29
Fruehauf Truck and Trailer Test in 80x120ft W.T. (looking at drag and fuel efficiency)
ARC-1988-AC88-0620-24
Fruehauf Truck and Trailer Test in 80x120ft W.T. (looking at drag and fuel efficiency)
ARC-1988-AC88-0620-23
Advanced Recovery Systems Parafoil test 80x120ft w.t. test-004
ARC-1988-AC88-0537-22
Advanced Recovery Systems Parafoil test 80x120ft w.t. test-004
ARC-1988-AC88-0537-31
Fruehauf Truck and Trailer Test in 80x120ft W.T. with LRLDV (looking at drag and fuel efficiency)
ARC-1988-AC88-0620-52
British royalty visits Ames; Prince Andrew, Duke of York on tour of 80x120ft Wind Tunnel
ARC-2002-ACD02-0028-11
British royalty visits Ames; Prince Andrew, Duke of York on tour in 80x120ft w.t.
ARC-2002-ACD02-0028-24
British royalty visits Ames; Prince Andrew, Duke of York on tour in 80x120ft w.t.
ARC-2002-ACD02-0028-25
British royalty visits Ames; Prince Andrew, Duke of York on tour in 80x120ft w.t.
ARC-2015-ACD02-0028-26
Ames Aerials: N-221B 80x120ft w.t. leg
ARC-1989-AC89-0234-27
Lockheed Martin Joint Strike Fighter (JSF) model LM-80-2, jet effects test 80x120ft. w.t. Test-80-0029 with Paul Askins
ARC-1997-AC97-0325-5
Lockheed Martin Joint Strike Fighter (JSF) model LM-80-2, jet effects test 80x120ft. w.t. Test-80-0029
ARC-1997-AC97-0325-17
Ames National Full-Scale Aerodynamic Complex - NFAC; 80x120ft Wind Tunnel, drive fans during reconstruction process
ARC-1986-AC86-8016-7
VISIT: ASTRONAUT CLASS OF 2000:  KAREN NYBERG, ALVIN DREW TOUR 80X120FT WITH OTHER CLASSMATES
ARC-2001-ACD01-0179-6
VISIT: ASTRONAUT CLASS OF 2000:  KAREN NYBERG, ALVIN DREW TOUR 80X120FT WITH OTHER CLASSMATES
ARC-2001-ACD01-0179-8
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
ARC-2009-ACD09-0053-006
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
ARC-2009-ACD09-0053-003
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
ARC-2009-ACD09-0053-012
VISIT: ASTRONAUT CLASS OF 2000:  KAREN NYBERG, ALVIN DREW TOUR 80X120FT WITH OTHER CLASSMATES
ARC-2001-ACD01-0179-5
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
ARC-2009-ACD09-0053-001
1/5th scale model of the 80x120ft w.t. in N-246
ARC-1974-A74-4515
VISIT: ASTRONAUT CLASS OF 2000:  KAREN NYBERG, ALVIN DREW TOUR 80X120FT WITH OTHER CLASSMATES   SHOWN WITH TOUR GUIDES SHEILA JOHNSON AND DAVID MORSE
ARC-2001-ACD01-0179-7
XV-15 Rotor Test Apparatus (RTA) flow visualization Hover test-80-0021 in 80x120ft w.t.
ARC-1996-AC96-0357-15
XV-15 Rotor Test Apparatus (RTA) flow visualization Hover test-80-0021 in 80x120ft w.t.  (rotor tip)
ARC-1996-AC96-0357-16
F-18 installed in 80x120ft w.t. for High Alpha Test-823 Phase II
ARC-1993-AC93-0150-105
F/A-18 (F-18) being moved to the 80x120ft w.t. for testing
ARC-1989-AC90-0001-14
F/A-18 (F-18) outside the 80x120ft w.t. inlet (it will be loaded in the tunnel for testing)
ARC-1989-AC90-0001-8
Ames Center Director S. Pete Worden visits the NFAC 80x120ft wind tunnel control room during a Parachute deployment test. Joe Sacco explains test procedure to Worden (on left).
ARC-2007-ACD07-0200-002
Mars Science Laboratory (MSL) parachuste test in the NASA Ames 80x120ft Subsonic Wind Tunnel at Moffett Field, Calif. (TR #22 - Phase 6) is the largest ever built to fly on an extraterrestrail mission. This image shows the qualification-test parachute beginning to open a few seconds after it was launched from a mortar into an 80-mile-per-hour (36-meter-per-second) wind.
ARC-2009-ACD09-0053-005
CALF/JAST X-32 test program:  the LSPM (Large Scale Powered Model), Lockheed's concept for a tri-service aircraft (Air Force, Navy, Marines) CALF (Common Affordable Lightweight Fighter) as part of the Department of Defense's Joint Advanced Strike Technology (JAST) is being tested in the 80x120ft w.t. test-930 with rear horizontal stabilizer
ARC-1996-AC95-0154-333
Mars Science Laboratory (MSL) parachuste test in the NASA Ames 80x120ft Subsonic Wind Tunnel at Moffett Field, Calif. (TR #22 - Phase 6) is the largest ever built to fly on an extraterrestrail mission. This image shows a duplicate qualification-test parachute inflated in a  80-mile-per-hour (36-meter-per-second) wind inside the test facility. It has 80 suspension lines, measures more that 50 meers (165 feet) in lenght, and opens to a diameter of nearly 16 meters (51 feet). Most the the orange and white fabric is nylon, though a small disk of heavier polyester is used near the vent in the apex of the canapy due to the higher stresses there.  It is designed to survive deployment at Mach 2.2 in the Martian atmosphere, where it will generate up to 65,000 pounds of drag force.
ARC-2009-ACD09-0053-008
Mars Science Laboratory (MSL) parachuste test in the NASA Ames 80x120ft Subsonic Wind Tunnel at Moffett Field, Calif. (TR #22 - Phase 6) is the largest ever built to fly on an extraterrestrail mission. This image shows a duplicate qualification-test parachute inflated in a  80-mile-per-hour (36-meter-per-second) wind inside the test facility. It has 80 suspension lines, measures more that 50 meers (165 feet) in lenght, and opens to a diameter of nearly 16 meters (51 feet). Most the the orange and white fabric is nylon, though a small disk of heavier polyester is used near the vent in the apex of the canapy due to the higher stresses there.  It is designed to survive deployment at Mach 2.2 in the Martian atmosphere, where it will generate up to 65,000 pounds of drag force.
ARC-2009-ACD09-0053-013
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Smoke test demo.
ARC-2010-ACD10-0020-065
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. LLNL's test piece is being installed on truck.
ARC-2010-ACD10-0020-034
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Smoke test demo with Ron Schoon, Navistar.
ARC-2010-ACD10-0020-082
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Smoke test demo.
ARC-2010-ACD10-0020-073
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Cab being lifted into the tunnel.
ARC-2010-ACD10-0020-013
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Smoke test demo with Ron Schoon, Navistar.
ARC-2010-ACD10-0020-079
Lawrence Livermore National Labs (LLNL), Navistar and the Department of Energy conduct tests in the NASA Ames National Full-scale Aerodynamic Complex 80x120_foot wind tunnel. The LLNL project is aimed at aerodynamic truck and trailer devices that can reduce fuel consumption at highway speed by 10 percent. Trailer being lifted into the tunnel.
ARC-2010-ACD10-0020-023
F-18 being installed in the NASA Ames Full-scale Aerodynamic Complex (NFAC) 80x120_foot wind tunnel test section for High Alpha Test-823 Phase II
ARC-1993-AC93-0150-114
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-1
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel. Gabriel and Sharon Lozano.
ARC-2010-ACD10-0029-027
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-2
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel. Lewis Braxton III, Deputy Director Ames Research Center speaker.
ARC-2010-ACD10-0029-013
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-6
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel. Mike Honda, U.S Congressman from California's 15th District
ARC-2010-ACD10-0029-030
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel. Mike Honda, U.S Congressman from California's 15th District
ARC-2010-ACD10-0029-018
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-4
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel.
ARC-2010-ACD10-0029-035
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. (microphone set up) Noise Reduction
ARC-1998-AC98-0261-7
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-5
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
ARC-1998-AC98-0261-3
Lawrence Livermore National Laboratories media Day  for their LLNL project aimed at aerodynamic truck and trailer devices. Tests are being preformed in the Ames Full-Scale Aerodynamic Complex 80x120 foot wind tunnel. Mike Honda, U.S Congressman from California's 15th District
ARC-2010-ACD10-0029-037
Sikorsky Rotor Systems Research Aircraft ' RSRA' (72-001 NASA-740) compound configuration in flight:  NASA Ames Research Center, Hangar and 40x 80x120ft W.T. in the background. Note:  Used in publication in Flight Research at Ames;  57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 fig. 132
ARC-1982-AC82-0253-11
(03/12/1976) 1/50 scale model of the 80x120 foot wind tunnel model (NFAC) in the test section of the 40x80 wind tunnel.  Model viewed from the west, mounted on a rotating ground board designed for this test. Ramp leading to ground board includes a generic building placed in front of the 80x120 inlet.
1/50 Scale Model Of The 80x120 Foot Wind Tunnel Model (NFAC) In The Test Section Of The 40x80 Wind Tunnel.
(03/12/1976) Overhead view of 1/50 scale model of the 80x120 foot wind tunnel model (NFAC) in the test section of the 40x80 wind tunnel at NASA Ames. Model mounted on a rotating ground board designed for this test.
1/50 Scale Model Of The 80X120 Foot Wind Tunnel Model (NFAC) In The Test Section Of The 40X80 Wind Tunnel At Nasa Ames.
(03/12/1976) 1/50 scale model of the 80x120 foot wind tunnel model (NFAC) in the test section of the 40x80 foot wind tunnel. Model mounted on a rotating ground board designed for this test, viewed from the west, oriented for North wind.
A76-0634. 1/50 Scale Model Of The 80X120 Foot Wind Tunnel Model (Nfac) In The Test Section Of The 40X80 Foot Wind Tunnel.