Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

Limit your search

Publication Date

Report Availability

10 reports

Description of the E-1 Tunnel, GDF

Author(s): C. J. Schueler
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1953-01
Report Number: AEDC TN 53-19
full text unavailable

Tests of 6-inch Hydraulic Relief Valve with Amplifier Ring

Author(s): James M. Langford
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report Number: AEDC TN 54-29
full text unavailable

Digital Manometer Reader for the Arnold Engineering Development Center

Author(s): Henry T. Chapek
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report Number: AEDC TR 54-32
full text unavailable

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): Charles E. Bond
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-01
Report Number: AEDC TN 54-45
full text unavailable

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): Bernhard H. Goethert
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1955-04
Report Number: AEDC TR 54-42
full text unavailable

On-Line Automatic Data Reduction Tunnel E-1 Gas Dynamics Facility

Author(s): C. L. Hall; R. E. Klautsch
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1956-04
Report Number: AEDC TN 56-4
full text unavailable

Experience With An Overexpanded Nozzle In A Low-Density, Hypervelocity Wind Tunnel

Author(s): J. Leith Potter and David E. Boylan
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-04
Report Number: AEDC TDR 62-85
full text unavailable

Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles

Author(s): J. R. Henson; J. E. Robertson
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report Number: AEDC TDR 62-7
full text unavailable

Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source

Author(s): C. T. Carman
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Report Number: AEDC TDR 62-15
full text unavailable

Flow-Field Investigation of a 0.0667-Scale Model of the X-15 Research Vehicle at Mach 4, 6, 8

Author(s): J. Rippey
Corporate Author: ARO, inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-10
Report Number: AEDC -TDR-201
full text unavailable