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Langley Research Center Media Archive
by NASA/Langley Research Center
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1/8th Scale shuttle external tank vibration test
Langley Research Center Media Archive
by NASA/Langley Research Center
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L85-9926: A 1/9th scale model of a Gulfstream business jet with advanced turboprop engine undergoing flutter tests in the Transonic Dynamics Tunnel. -- Photograph published in Winds of Change, 75th Anniversary of NASA, (page 128), by James Schultz.
Topic: MODEL AIRCRAFT. -- SCALE MODELS.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 32

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 28

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 35

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 33

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 32

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 24

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 25

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 21

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 27

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 49

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 28

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Drop test at the drop tower. Photographed at the Impact Dynamics Research Facility, building 1297.
Topic: AIRCRAFT STRUCTURES -- ENERGY ABSORPTION
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on: 12/13/1999. -- People in photographs include: Ethel Wescott, Heide Ellis, and James H. Ogiba.
Topic: AWARDS -- PERSONNEL -- EMPLOYEE RELATION
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on: 12/13/1999. -- People in photographs include: Ethel Wescott, Heide Ellis, and James H. Ogiba.
Topic: AWARDS -- PERSONNEL -- EMPLOYEE RELATION
Langley Research Center Media Archive
by NASA/Langley Research Center
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106B Flight Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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11 Foot Hypertonic Tunnel building 1229
Langley Research Center Media Archive
by NASA/Langley Research Center
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11 Foot Hypertonic Tunnel building 1229
Langley Research Center Media Archive
by NASA/Langley Research Center
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11 Foot Hypertonic Tunnel building 1229
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed October 1998. -- 11% scale of the F-18 E/F Free Flight model in the 14 x 22 Wind Tunnel. Photographed October 1998.
Topic: AIRCRAFT MODELS -- SCALE MODELS -- F-18
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed October 1998. -- 11% scale of the F-18 E/F Free Flight model in the 14 x 22 Wind Tunnel. Photographed October 1998.
Topic: AIRCRAFT MODELS -- SCALE MODELS -- F-18
Langley Research Center Media Archive
by NASA/Langley Research Center
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1146 Scaffolding
Langley Research Center Media Archive
by NASA/Langley Research Center
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1146 Scaffolding
Langley Research Center Media Archive
by NASA/Langley Research Center
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Image L86-4835 is available as an electronic file from the photo lab. -- Aerial views of the 12 Foot Tunnel showing motor room, Spin Tunnel and Full Scale Tunnel. Views of fan blade in tunnel.
Langley Research Center Media Archive
by NASA/Langley Research Center
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14x22 Foot Wind Tunnel Acoustic Treatment, Fan Model Close up and long shots -- 12 Inch ADP Demonstrator Acoustic Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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14x22 Foot Wind Tunnel Acoustic Treatment, Fan Model Close up and long shots -- 12 Inch ADP Demonstrator Acoustic Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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14x22 Foot Wind Tunnel Acoustic Treatment, Fan Model Close up and long shots -- 12 Inch ADP Demonstrator Acoustic Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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14x22 Foot Wind Tunnel Acoustic Treatment, Fan Model Close up and long shots -- 12 Inch ADP Demonstrator Acoustic Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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14x22 Foot Wind Tunnel Acoustic Treatment, Fan Model Close up and long shots -- 12 Inch ADP Demonstrator Acoustic Test
Langley Research Center Media Archive
by NASA/Langley Research Center
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Advanced Ducted Propeller (ADP). -- 12 inch ADP fan acoustic/aero test. -- To view image L95-3094, see URL. -- 12 inch ADP demonstrator in 14x22 Foot Wind Tunnel has been reconfigured for acoustic testing.
Topic: WIND TUNNELS. -- WIND TUNNEL TESTS. -- A
Langley Research Center Media Archive
by NASA/Langley Research Center
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Advanced Ducted Propeller (ADP). -- 12 inch ADP fan acoustic/aero test. -- To view image L95-3094, see URL. -- 12 inch ADP demonstrator in 14x22 Foot Wind Tunnel has been reconfigured for acoustic testing.
Topic: WIND TUNNELS. -- WIND TUNNEL TESTS. -- A
Langley Research Center Media Archive
by NASA/Langley Research Center
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Advanced Ducted Propeller (ADP). -- 12 inch ADP fan acoustic/aero test. -- To view image L95-3094, see URL. -- 12 inch ADP demonstrator in 14x22 Foot Wind Tunnel has been reconfigured for acoustic testing.
Topic: WIND TUNNELS. -- WIND TUNNEL TESTS. -- A
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 27

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 31

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 30

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 31

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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eye 22

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 30

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Photographed on: 06/01/98. -- Mach 10 (31") heater, tube bundle, control room, transformer. Mach 6 (15") heater, control room. Air switch assembly. Building 1251 A.
Topic: WIND TUNNEL DRIVES -- WIND TUNNELS -- TE
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on 12/10/96. -- 12.5 Hyper-X Blade/Sting Interference Model in the NASA Langley 20-Inch Mach Tunnel. Researchers include Dr. Scott D. Holland and William C. Woods of the Aerothermodynamics Branch/Aero-and Gas-Dynamics Division. This model was designed to provide the support hardware interference corrections to the aerodynamic data. The model was configured to permit blade mounting both with and without a dummy sting (to determine the increment due to the presence of the sting) and...
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on 12/10/96. -- 12.5 Hyper-X Blade/Sting Interference Model in the NASA Langley 20-Inch Mach Tunnel. Researchers include Dr. Scott D. Holland and William C. Woods of the Aerothermodynamics Branch/Aero-and Gas-Dynamics Division. This model was designed to provide the support hardware interference corrections to the aerodynamic data. The model was configured to permit blade mounting both with and without a dummy sting (to determine the increment due to the presence of the sting) and...
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
image

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Photographed on 12/10/96. -- 12.5 Hyper-X Blade/Sting Interference Model in the NASA Langley 20-Inch Mach Tunnel. Researchers include Dr. Scott D. Holland and William C. Woods of the Aerothermodynamics Branch/Aero-and Gas-Dynamics Division. This model was designed to provide the support hardware interference corrections to the aerodynamic data. The model was configured to permit blade mounting both with and without a dummy sting (to determine the increment due to the presence of the sting) and...
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 31

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Photographed on 12/10/96. -- 12.5 Hyper-X Blade/Sting Interference Model in the NASA Langley 20-Inch Mach Tunnel. Researchers include Dr. Scott D. Holland and William C. Woods of the Aerothermodynamics Branch/Aero-and Gas-Dynamics Division. This model was designed to provide the support hardware interference corrections to the aerodynamic data. The model was configured to permit blade mounting both with and without a dummy sting (to determine the increment due to the presence of the sting) and...
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on 10/28/99. -- 12.5% Hyper-X Research Vehicle (HXRV) model is shown in the 31-Inch Mach 10 Tunnel. The model was designed to provide fine control increments to determine hypersonic elevator, aileron, and rudder control effectiveness. Researchers include: Dr. Scott D. Holland, and William C. Woods. Photographed in the 31-Inch Mach 10 Tunnel, building 1251.
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on 10/28/99. -- 12.5% Hyper-X Research Vehicle (HXRV) model is shown in the 31-Inch Mach 10 Tunnel. The model was designed to provide fine control increments to determine hypersonic elevator, aileron, and rudder control effectiveness. Researchers include: Dr. Scott D. Holland, and William C. Woods. Photographed in the 31-Inch Mach 10 Tunnel, building 1251.
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
image

eye 54

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Photographed on 10/28/99. -- 12.5% Hyper-X Research Vehicle (HXRV) model is shown in the 31-Inch Mach 10 Tunnel. The model was designed to provide fine control increments to determine hypersonic elevator, aileron, and rudder control effectiveness. Researchers include: Dr. Scott D. Holland, and William C. Woods. Photographed in the 31-Inch Mach 10 Tunnel, building 1251.
Topic: WIND TUNNEL MODELS -- AIRCRAFT MODELS --
Langley Research Center Media Archive
by NASA/Langley Research Center
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1251 Personnel
Langley Research Center Media Archive
by NASA/Langley Research Center
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139-13 Orbiter and tank
Langley Research Center Media Archive
by NASA/Langley Research Center
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Image L69-991 is available as an electronic file from the photo lab. See URL. -- Photographed on 02/24/69. -- Construction of 14 by 22-Foot Wind Tunnel: The 14 by 22-foot Wind Tunnel is used to study low-speed aerodynamics. Both powered and unpowered models of various fixed- and rotary-wing aircraft are tested in this facility which can be operated as a closed test section with slotted walls or as one or more open configurations when the sidewalls and ceiling are removed to allow extra test...
Topic: WIND TUNNELS.
Langley Research Center Media Archive
by NASA/Langley Research Center
image

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Photographed on 05/09/68. -- Construction of 14 by 22-foot wind tunnel: The 14 by 22-foot Wind Tunnel is used to study low-speed aerodynamics. Both powered and unpowered models of various fixed- and rotary-wing aircraft are tested in this facility which can be operated as a closed test section with slotted walls or as one or more open configurations when the sidewalls and ceiling are removed to allow extra test capabilities, such as flow visualization and acoustics testing. It was built in 1968...
Topic: WIND TUNNELS.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Image L68-6965 is available as an electronic file from the photo lab. See URL. -- Photographed on 07/01/68. -- Construction of 14 by 22-foot wind tunnel: The 14 by 22-foot Wind Tunnel is used to study low-speed aerodynamics. Both powered and unpowered models of various fixed- and rotary-wing aircraft are tested in this facility which can be operated as a closed test section with slotted walls or as one or more open configurations when the sidewalls and ceiling are removed to allow extra test...
Topic: WIND TUNNELS.
Langley Research Center Media Archive
by NASA/Langley Research Center
image

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Image L70-7482 is available as an electronic file from the photo lab. See URL. -- Photographed on 11/23/70. -- Shop preparing models for testing in 14 by 22-foot Wind Tunnel: The 14 by 22-foot Wind Tunnel is used to study low-speed aerodynamics. Both powered and unpowered models of various fixed- and rotary-wing aircraft are tested in this facility which can be operated as a closed test section with slotted walls or as one or more open configurations when the sidewalls and ceiling are removed...
Topic: WIND TUNNELS.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Photographed on 05/21/68. -- Image L68-5099 is available as an electronic file from the photo lab. See URL. -- Construction of 14 by 22-foot wind tunnel: The 14 by 22-Foot Wind Tunnel is used to study low-speed aerodynamics. Both powered and unpowered models of various fixed- and rotary-wing aircraft are tested in this facility which can be operated as a closed test section with slotted walls or as one or more open configurations when the sidewalls and ceiling are removed to allow extra test...
Topic: WIND TUNNELS. -- FACILITIES.
Langley Research Center Media Archive
by NASA/Langley Research Center
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14 x 22 Drive Motor
Langley Research Center Media Archive
by NASA/Langley Research Center
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Pre and post cleaning.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Pre and post cleaning.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Pre and post cleaning.
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by NASA/Langley Research Center
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Pre and post cleaning.
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by NASA/Langley Research Center
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Pre and post cleaning.
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by NASA/Langley Research Center
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Pre and post cleaning.
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by NASA/Langley Research Center
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Pre and post cleaning.
Langley Research Center Media Archive
by NASA/Langley Research Center
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Pre and post cleaning.
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by NASA/Langley Research Center
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Pre and post cleaning.
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Pre and post cleaning.
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Pre and post cleaning.