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Description of the E-1 Tunnel, GDF
Author(s): Schueler, C. J.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1953-01
Report number: AEDC TN 53-19
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Digital Manometer Reader for the Arnold Engineering Development Center
Author(s): Chapek, Henry T.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report number: AEDC TR 54-32
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Calibration of the Gas Dynamics Facility Tunnel with Supply Pressures up to 60 psia and Mach Numbers from 1.4 to 2.5
Author(s): Bond, Charles E.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report number: AEDC TN 54-45
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Influence of Plenum-chamber Suction and Wall Convergence on the Mach Number Distribution in Patially Open Test Sections of Wind Tunnels at Subsonic and Supersonic Speeds
Author(s): Goethert, Bernhard H.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-04
Report number: AEDC TR 54-42
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Tests of 6-inch Hydraulic Relief Valve with Amplifier Ring
Author(s): Langford, James M.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report number: AEDC TN 54-29
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On-Line Automatic Data Reduction Tunnel E-1 Gas Dynamics Facility
Author(s): Hall, C. L., Klautsch, R. E.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1956-04
Report number: AEDC TN 56-4
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Experience With An Overexpanded Nozzle In A Low-Density, Hypervelocity Wind Tunnel
Author(s): Potter, J. Leith, Boylan, David E.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-04
Report number: AEDC TDR 62-85
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Flow-Field Investigation of a 0.0667-Scale Model of the X-15 Research Vehicle at Mach 4, 6, 8
Author(s): Rippey, J.
Corporate Author(s): ARO, inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-10
Report number: AEDC -TDR-201
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Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles
Author(s): Henson, J. R., Robertson, J. E.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report number: AEDC TDR 62-7
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Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source
Author(s): Carman, C. T.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Report number: AEDC TDR 62-15

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