Chief Engineer of the Marine Corps Jeannette Evans-Morgis
Chief Engineer of the Marine Corps Jeannette Evans-Morgis (center) and Mark Jackson, assistant portfolio manager–Engineering for Network and Infrastructure, demonstrate the FitLight Trainer April 6, at Marine C... More
Chicago-area team members build strength through community outreach
Chicago-area Defense Contract Management Agency team members recently partnered with a local charity to package meals for hungry children around the world. Fourteen employees volunteered two hours of personal t... More
160529-N-WI365-033 ULAANBAATAR, Mongolia (May 29, 2016)
160529-N-WI365-033 ULAANBAATAR, Mongolia (May 29, 2016) – U.S. Army Spc. Israa Kako-Gehring, assigned to 297th Military Police Company of the Alaska Army National Guard, reads about an ancient artifact in the M... More
The U.S. Army Corps of Engineers Norfolk District assists
The U.S. Army Corps of Engineers Norfolk District assists Newport News Public Schools at the NNPS Engineering Design Challenge held at Newsome Park Elementary School, Newport News, Va., Nov. 2, 2018. Fourth and... More
Students from Bolden Elementary/Middle School aboard
Students from Bolden Elementary/Middle School aboard Laurel Bay browse through items during Career Day at the school’s gymnasium Jan. 22. The day was part of a familiarization for the students in careers that t... More
Full-Scale Tunnel (FST), NASA history collection
Pile driving for foundation of Full-Scale Tunnel (FST). In 1924, George Lewis, Max Munk and Fred Weick began to discuss an idea for a wind tunnel large enough to test a full-scale propeller. Munk sketched out a... More
11-Inch High-Speed Tunnel. NASA public domain image colelction.
Construction of 5 Foot Vertical Wind Tunnel. The 5 Foot Vertical Wind Tunnel was built to study spinning characteristics of aircraft. It was an open throat tunnel capable of a maximum speed of 80 mph. NACA engi... More
NACA-A Look Back, NASA history collection
Many of Langley Laboratory's early experiments focused on ways to reduce aircraft drag. One method was to place a cowling or covering over the engine cylinder heads, much like the hood over the engine of a car.... More
11-Inch High-Speed Tunnel. NASA public domain image colelction.
Construction of 5 Foot Vertical Wind Tunnel. The 5 Foot Vertical Wind Tunnel was built to study spinning characteristics of aircraft. It was an open throat tunnel capable of a maximum speed of 80 mph. NACA engi... More
Full Scale Tunnel (FST) and Seaplane Tow Channel
Aerial and ground views of the overall construction of Full-Scale Tunnel (FST) and the Seaplane Tow Channel. In November 1929, Smith DeFrance submitted his recommendations for the general design of the Full Sca... More
Test of 4" x 20" Clark-Y airfoil model in FST
Test of 4" x 20" Clark-Y airfoil model in Full-Scale Tunnel (FST). On June 26, 1929, Elton W. Miller wrote to George W. Lewis proposing the construction of a model of the full-scale tunnel. "The excellent energ... More
Meeting of the Main Committee of the NACA
The Main Committe of the NACA met in Washington,D.C., twice a year, the annual meeting being held in October and the semiannual meeting in April. Among the matters discussed at this semiannual meeting on 18 Apr... More
Full Scale Tunnel (FST), NASA history collection
Construction of Full-Scale Tunnel (FST). In November 1929, Smith DeFrance submitted his recommendations for the general design of the Full Scale Wind Tunnel. The last on his list concerned the division of labor... More
Test of 4" x 20" Clark-Y airfoil model in FST
Test of 4" x 20" Clark-Y airfoil model in Full-Scale Tunnel (FST). On June 26, 1929, Elton W. Miller wrote to George W. Lewis proposing the construction of a model of the full-scale tunnel. "The excellent energ... More
Full Scale Tunnel (FST), NASA history collection
Construction of Full-Scale Tunnel (FST). In November 1929, Smith DeFrance submitted his recommendations for the general design of the Full Scale Wind Tunnel. The last on his list concerned the division of labor... More
Full Scale Tunnel (FST) and Seaplane Tow Channel
Aerial and ground views of the overall construction of Full-Scale Tunnel (FST) and the Seaplane Tow Channel. In November 1929, Smith DeFrance submitted his recommendations for the general design of the Full Sca... More
Full Scale Wind Tunnel, NASA history collection
View of the 30 x 60 Full Scale Tunnel's huge (434 by 222 feet, and 90 feet high) exterior from the Little Back River in October 1930. NASA Identifier: L4933
7 x 10-Foot Atmospheric Wind Tunnel (AWT)
Smoke generator for 7 x 10-Foot Atmospheric Wind Tunnel (AWT) (left center); Force Test Set-Up in the center. In 1928, the NACA decided to replace its original Atmospheric Wind Tunnel (AWT #1) with two tunnels-... More
7 x 10-Foot Atmospheric Wind Tunnel (AWT)
Smoke generator for 7 x 10-Foot Atmospheric Wind Tunnel (AWT) (left center); Force Test Set-Up in the center. In 1928, the NACA decided to replace its original Atmospheric Wind Tunnel (AWT #1) with two tunnels-... More
24-Inch High Speed Tunnel (24-Inch HST)
24-Inch High Speed Tunnel (24-Inch HST): Construction of the foundation for the tunnel. Construction was authorized in 1933 and was built using funds from the Federal Public Works Administration (PWA). The init... More
24-Inch High Speed Tunnel (24-Inch HST)
24-Inch High Speed Tunnel (24-Inch HST): Construction of the foundation for the tunnel. Construction was authorized in 1933 and was built using funds from the Federal Public Works Administration (PWA). The init... More
15-Foot Spin Tunnel, NASA history collection
Constructing the forms for the foundation of the 15-Foot Spin Tunnel. Charles Zimmerman was given the assignment to design and build a larger spin tunnel that would supplant the 5-foot Vertical Wind Tunnel. Aut... More
24-Inch High Speed Tunnel (24-Inch HST)
24-Inch High Speed Tunnel (24-Inch HST): Construction of the foundation for the tunnel. Construction was authorized in 1933 and was built using funds from the Federal Public Works Administration (PWA). The init... More
15-Foot Spin Tunnel, NASA history collection
Constructing the forms for the foundation of the 15-Foot Spin Tunnel. Charles Zimmerman was given the assignment to design and build a larger spin tunnel that would supplant the 5-foot Vertical Wind Tunnel. Aut... More
24-Inch High Speed Tunnel (24-Inch HST)
24-Inch High Speed Tunnel (24-Inch HST): Construction of the foundation for the tunnel. Construction was authorized in 1933 and was built using funds from the Federal Public Works Administration (PWA). The init... More
NACA-A Look Back, NASA history collection
Amelia Earhart front row, center on the steps of Langley Research Building in 1928 before a tour. Legend has it that, during the tour, part of her raccoon fur coat was sucked into a high speed wind tunnel. Imag... More
Two-Dimensional Low-Turbulence Tunnel
Construction of the wood frame for the Two-Dimensional Low-Turbulence Tunnel. The Two-Dimensional Low-Turbulence Tunnel was originally called the Refrigeration or "Ice" tunnel because it was intended to support... More
Two-Dimensional Low-Turbulence Tunnel
Manometer for the Two-Dimensional Low-Turbulence Tunnel. The Two-Dimensional Low-Turbulence Tunnel was originally called the Refrigeration or "Ice" tunnel because it was intended to support research on aircraft... More
Two-Dimensional Low-Turbulence Tunnel
Construction of the Two-Dimensional Low-Turbulence Tunnel. The Two-Dimensional Low-Turbulence Tunnel was originally called the Refrigeration or "Ice" tunnel because it was intended to support research on aircra... More
Two-Dimensional Low-Turbulence Tunnel
Construction of the Two-Dimensional Low-Turbulence Tunnel. The Two-Dimensional Low-Turbulence Tunnel was originally called the Refrigeration or "Ice" tunnel because it was intended to support research on aircra... More
USS Enterprise (CV 6) landing an aircraft while supporting
USS Enterprise (CV 6) landing an aircraft while supporting the Gilberts Operation in November 1943. (U.S. Naval History and Heritage Command Photograph.)
BUILDING CONSTRUCTION ALTITUDE WIND TUNNEL
BUILDING CONSTRUCTION ALTITUDE WIND TUNNEL NASA Identifier: C-1942-1166
BUILDING CONSTRUCTION ALTITUDE WIND TUNNEL
BUILDING CONSTRUCTION ALTITUDE WIND TUNNEL NASA Identifier: C-1942-1165
VIEW OF ALTITUDE WIND TUNNEL DURING CONSTRUCTION
VIEW OF ALTITUDE WIND TUNNEL DURING CONSTRUCTION NASA Identifier: C-1943-1521
ALTITUDE WIND TUNNEL PROPELLER LAMINATED WOOD CONSTRUCTION
ALTITUDE WIND TUNNEL PROPELLER LAMINATED WOOD CONSTRUCTION NASA Identifier: C-1943-1848
VIEW OF ALTITUDE WIND TUNNEL DURING CONSTRUCTION
VIEW OF ALTITUDE WIND TUNNEL DURING CONSTRUCTION NASA Identifier: C-1943-1520
EXHAUSTER AND WIND TUNNEL DRIVE EQUIPMENT - KISSLE'S DRAWING
EXHAUSTER AND WIND TUNNEL DRIVE EQUIPMENT - KISSLE'S DRAWING NASA Identifier: C-1943-2020
WIND TUNNEL VIEW - KUNEAR ROLLING DOOR
WIND TUNNEL VIEW - KUNEAR ROLLING DOOR NASA Identifier: C-1944-4804
COPY OF WIND TUNNEL DRAWING - Public domain architectural drawing
COPY OF WIND TUNNEL DRAWING NASA Identifier: C-1944-5142
CONSTRUCTION OF WIND TUNNEL, NASA history collection
CONSTRUCTION OF WIND TUNNEL NASA Identifier: C-1944-6707 Public domain photograph of the train tunnel, railroad, train track, free to use, no copyright restrictions image - Picryl description
ALTITUDE WIND TUNNEL (AWT) PUBLICITY WITH MODEL INTERIOR THROAT SECTIO...
ALTITUDE WIND TUNNEL (AWT) PUBLICITY WITH MODEL INTERIOR THROAT SECTION NASA Identifier: C-1944-3991
PUBLICITY FOR WIND TUNNEL, NASA history collection
PUBLICITY FOR WIND TUNNEL NASA Identifier: C-1944-7427
WIND TUNNEL TEST SECTION, NASA history collection
WIND TUNNEL TEST SECTION NASA Identifier: C-1944-6305 Public domain photograph of the train tunnel, railroad, train track, free to use, no copyright restrictions image - Picryl description
WIND TUNNEL TORQUE STAND ON HANGAR RAMP FROM NORTHWEST/NORTHEAST SIDE/...
WIND TUNNEL TORQUE STAND ON HANGAR RAMP FROM NORTHWEST/NORTHEAST SIDE/POWER PLANT FROM NORTHEAST/JET PROPULSION STATIC LAB/ERB FROM NORTHEAST/SUPERCHARGER WING FROM NORTHWEST NASA Identifier: C-1945-12096
WIND TUNNEL GROUP, NASA history collection
WIND TUNNEL GROUP NASA Identifier: C-1945-10855
PUBLICITY - WIND TUNNEL AT NIGHT
PUBLICITY - WIND TUNNEL AT NIGHT NASA Identifier: C-1945-9514
POWER HOUSE ICING TUNNEL TO WIND TUNNEL BUILDING GROUP
POWER HOUSE ICING TUNNEL TO WIND TUNNEL BUILDING GROUP NASA Identifier: C-1945-13017
WIND TUNNEL TORQUE STAND ON HANGAR RAMP FROM NORTHWEST/FROM NORTHEAST ...
WIND TUNNEL TORQUE STAND ON HANGAR RAMP FROM NORTHWEST/FROM NORTHEAST SIDE/POWER PLANT FROM NORTHEAST/JET PROPULSION STATIC LAB/ERB FROM NORTHEAST/SUPERCHARGER WING FROM NORTHWEST NASA Identifier: C-1945-12097
PUBLICITY - WIND TUNNEL AT NIGHT
PUBLICITY - WIND TUNNEL AT NIGHT NASA Identifier: C-1945-9513
PUBLICITY WIND TUNNEL ROOF AND HANGAR APRON
PUBLICITY WIND TUNNEL ROOF AND HANGAR APRON NASA Identifier: C-1945-10527
WIND TUNNEL BUILDING FROM NORTHEAST CORNER
WIND TUNNEL BUILDING FROM NORTHEAST CORNER NASA Identifier: C-1945-12067
PUBLICITY WIND TUNNEL ROOF AND HANGAR APRON
PUBLICITY WIND TUNNEL ROOF AND HANGAR APRON NASA Identifier: C-1945-10529
1946, NASA history collection, Glenn Research Center
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1946-15820
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT - EXHAUST GAS ...
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT - EXHAUST GAS COOLER IN THE NEW WING OF THE ENGINE RESEARCH BUILDING NASA Identifier: C-1946-15822
RAM JET INSTALLATION IN THE ALTITUDE WIND TUNNEL AWT
RAM JET INSTALLATION IN THE ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1946-14241
1946, NASA history collection, Glenn Research Center
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT - FINAL REFRIGERATION UNIT IN THE ENGINE RESEARCH BUILDING ERB FOR REFRIGERATION COMBUSTION AIR NASA Identifier: C-1946-15823
RAM JET INSTALLATION IN THE ALTITUDE WIND TUNNEL AWT
RAM JET INSTALLATION IN THE ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1946-14244
1946, NASA history collection, Glenn Research Center
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT - FINAL REFRIGERATION UNIT IN THE ENGINE RESEARCH BUILDING ERB FOR REFRIGERATION COMBUSTION AIR NASA Identifier: C-1946-15821
1946, NASA history collection, Glenn Research Center
INSULATION AND ASSEMBLY OF THE ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1946-15817
1946, NASA history collection, Glenn Research Center
RAM JET INSTALLATION IN THE ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1946-14248
Highest Honors for Game-Changing Innovation
In 1947, the Collier Trophy was awarded to John Stack of Langley Memorial Aeronautical Laboratory for research to determine the physical laws affecting supersonic flight. Lawrence D. Bell and Chuck Yeager also ... More
DE-ICING SETUP ON X24C MODEL MOUNTED IN ALTITUDE WIND TUNNEL AWT
DE-ICING SETUP ON X24C MODEL MOUNTED IN ALTITUDE WIND TUNNEL AWT NASA Identifier: C-1947-18308
HIGH SPEED MOVIES THROUGH SCHLIEREN EQUIPMENT 18X18 INCH SUPERSONIC WI...
HIGH SPEED MOVIES THROUGH SCHLIEREN EQUIPMENT 18X18 INCH SUPERSONIC WIND TUNNEL SHADOWGRAPH OF 18X18 INCH SUPERSONIC WIND TUNNEL WITH JIM CONNORS NASA Identifier: C-1948-22209
HIGH SPEED MOVIES THROUGH SCHLIEREN EQUIPMENT 18X18 INCH SUPERSONIC WI...
HIGH SPEED MOVIES THROUGH SCHLIEREN EQUIPMENT 18X18 INCH SUPERSONIC WIND TUNNEL SHADOWGRAPH OF 18X18 INCH SUPERSONIC WIND TUNNEL WITH JIM CONNORS NASA Identifier: C-1948-22208
8X6 FOOT SUPERSONIC WIND TUNNEL CONTROL ROOM IN FULL ACTION TAKING DAT...
8X6 FOOT SUPERSONIC WIND TUNNEL CONTROL ROOM IN FULL ACTION TAKING DATA NASA Identifier: C-1949-24643
AXIAL FLOW COMPRESSOR IN THE 8X6 FOOT SUPERSONIC WIND TUNNEL - ELECTRI...
AXIAL FLOW COMPRESSOR IN THE 8X6 FOOT SUPERSONIC WIND TUNNEL - ELECTRIC MOTORS OF 87,000 HORSEPOWER DRIVE THIS HUGE COMPRESSOR TO PRODUCE 1300 MILE PER HOUR AIRSPEEDS - THE 2 HALVES OF THE 18 FOOT DIAMETER CASI... More
AERIAL VIEW OF THE 8X6 FOOT SUPERSONIC WIND TUNNEL
AERIAL VIEW OF THE 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1949-24971
SCHLIEREN BOARD SETUP IN 18X18 INCH SUPERSONIC WIND TUNNEL
SCHLIEREN BOARD SETUP IN 18X18 INCH SUPERSONIC WIND TUNNEL NASA Identifier: C-1949-23018
RM-10 INSTALLATION IN THE 8X6 FOOT WIND TUNNEL - OPERATIONS ENGINEER R...
RM-10 INSTALLATION IN THE 8X6 FOOT WIND TUNNEL - OPERATIONS ENGINEER RAYMOND J KARABINUS AND TECHNICIAN GRADY S SPEER MAKE FINAL CHECK OF BOUNDARY LAYER RAKES AT READ OF STING MOUNTED LANGLEY RESEARCH MISSILE M... More
MANOMETER BOARD SETUP IN THE 18X18 INCH SUPERSONIC WIND TUNNEL
MANOMETER BOARD SETUP IN THE 18X18 INCH SUPERSONIC WIND TUNNEL NASA Identifier: C-1949-23011
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25074
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25068
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25072
CONSTRUCTION OF ACOUSTICAL HOUSING ADDITION TO 8X6 FOOT SUPERSONIC WIN...
CONSTRUCTION OF ACOUSTICAL HOUSING ADDITION TO 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-26415
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25075
NOISE ELIMINATION TESTS OF 8X6 FOOT SUPERSONIC WIND TUNNEL PHOTOGRAPHE...
NOISE ELIMINATION TESTS OF 8X6 FOOT SUPERSONIC WIND TUNNEL PHOTOGRAPHED FOR THE CLEVELAND PLAIN DEALER NEWSPAPER ARTICLE NASA Identifier: C-1950-25103
Unitary Plan Supersonic Tunnel, NASA history collection
Unitary Plan Supersonic Tunnel: In this aerial photograph of construction in the early 1950s, the return air passages are shown in the front, left portion. This area was later covered with walls and a roof so t... More
CLEANING PITOT TUBE OF 16 INCH RAM JET IN THE 8X6 FOOT WIND TUNNEL
CLEANING PITOT TUBE OF 16 INCH RAM JET IN THE 8X6 FOOT WIND TUNNEL NASA Identifier: C-1950-25677
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25070
CONSTRUCTION OF ACOUSTICAL HOUSING ADDITION TO 8X6 FOOT SUPERSONIC WIN...
CONSTRUCTION OF ACOUSTICAL HOUSING ADDITION TO 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-26414
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25066
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25071
NACA 16 INCH RAM JET IN 8X6 FOOT SUPERSONIC WIND TUNNEL
NACA 16 INCH RAM JET IN 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25776
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25069
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25065
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25073
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL NASA Identifier: C-1950-25067
NOISE ELIMINATION TESTS OF 8X6 FOOT SUPERSONIC WIND TUNNEL PHOTOGRAPHE...
NOISE ELIMINATION TESTS OF 8X6 FOOT SUPERSONIC WIND TUNNEL PHOTOGRAPHED FOR THE CLEVELAND PLAIN DEALER NEWSPAPER ARTICLE NASA Identifier: C-1950-25104
Engineering Greatness: Rear Adm. Erroll M. Brown
Engineered for Greatness: Erroll M. Brown By Petty Officer Joshua Canup An engineer is someone who takes many different parts and puts them together in working order, recognizing the worth and placement of each... More
Highest Honors for Game-Changing Innovation
In 1951, the Collier Trophy was awarded again to John Stack and associates at the Langley Memorial Aeronautical Laboratory for the development and use of the slotted-throat wind tunnel. Stack, head of Compressi... More
COMPUTER IN THE 8X6 FOOT WIND TUNNEL
COMPUTER IN THE 8X6 FOOT WIND TUNNEL NASA Identifier: C-1951-27174
MANOMETER IN THE 8X6 FOOT WIND TUNNEL BASEMENT
MANOMETER IN THE 8X6 FOOT WIND TUNNEL BASEMENT NASA Identifier: C-1951-27175
16 INCH RAM JET IN TEST SECTION OF THE 8X6 FOOT WIND TUNNEL
16 INCH RAM JET IN TEST SECTION OF THE 8X6 FOOT WIND TUNNEL NASA Identifier: C-1951-28473
LEWIS HISTORICAL PICTURES - Edward, Duke of Windsor tours the 8x6 Supe...
LEWIS HISTORICAL PICTURES - Edward, Duke of Windsor tours the 8x6 Supersonic Wind Tunnel with Ray Sharp on May 22, 1951 NASA Identifier: C-1984-2302
NACA AUTOMATIC DATA RECORDER IN THE 8X6 FOOT WIND TUNNEL BASEMENT
NACA AUTOMATIC DATA RECORDER IN THE 8X6 FOOT WIND TUNNEL BASEMENT NASA Identifier: C-1952-31565
4 INCH RAM JET IN THE 18X18 INCH SUPERSONIC WIND TUNNEL MACH NO. 4
4 INCH RAM JET IN THE 18X18 INCH SUPERSONIC WIND TUNNEL MACH NO. 4 NASA Identifier: C-1952-29161
RAM JET RJM-2 MODEL IN THE TEST SECTION OF THE 8X6 FOOT WIND TUNNEL
RAM JET RJM-2 MODEL IN THE TEST SECTION OF THE 8X6 FOOT WIND TUNNEL NASA Identifier: C-1952-29143
NACA AUTOMATIC DATA RECORDER IN THE 8X6 FOOT WIND TUNNEL BASEMENT
NACA AUTOMATIC DATA RECORDER IN THE 8X6 FOOT WIND TUNNEL BASEMENT NASA Identifier: C-1952-31564
IBM CALCULATOR IN THE 8X6 FOOT WIND TUNNEL BASEMENT
IBM CALCULATOR IN THE 8X6 FOOT WIND TUNNEL BASEMENT NASA Identifier: C-1952-30194
RAM JET RJM-1 MODEL IN THE TEST SECTION OF THE 8X6 FOOT WIND TUNNEL
RAM JET RJM-1 MODEL IN THE TEST SECTION OF THE 8X6 FOOT WIND TUNNEL NASA Identifier: C-1952-29217