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.

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14 reports

Reduction of Drag Due to Lift at Supersonic Speeds

Author(s): Graham, E. W.
Corporate Author: Douglas Aircraft Company
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-08
Report Number: WADC TR 54-524 Part 2
full text available

An Analogue Series Computer

Author(s): Scherberg, Max G.
Corporate Author: Aeronautical Research Laboratory
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-08
Report Number: WADC TR 54-174
full text available

Reduction Of Drag Due To Lift At Supersonic Speeds

Author(s): Graham, E. W.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-04
Report Number: WADC TR 54-524 Part 1
full text available

Flight Evaluations Of Variable Short Period And Phugoid Characteristics In A B-26

Author(s): Newell, Fred
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-594
full text available

Metal And Self-bonded Silicon Carbide

Author(s): Alliegro, R. A.
Corporate Author: New York State College Of Ceramics
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-01
Report Number: WADC TR 54-38
full text available

Series Solution Of Laminar Incompressible Mixing Of Two Streams with Different Velocities

Author(s): Eldrenkamp, L. G.
Corporate Author: Illinois U.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-05
Report Number: WADC TR 54-275
full text available

Princeton Helium Hypersonic Tunnel And Preliminary Results Above M=11

Author(s): Bogdonoff, S. M.
Corporate Author: James Forrestal Research Foundation, Princeton University
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-07
Report Number: WADC TR 54-124
full text available

Schlieren System for Perforated Wall Type Transonic Wind Tunnels

Author(s): Behun, Eugene
Corporate Author: United Aircraft Corp.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-511
full text available

Delayed Failure And Hydrogen Embrittlement In Steel

Author(s): Frohmberg, R. P.
Corporate Author: Case Institute Of Technology
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-06
Report Number: WADC TR 54-320
full text available

Determination Of Residual Stresses By Indentation Methods

Author(s): Bareiss, Robert A.
Corporate Author: Lessells And Associates, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-615
full text available

Prestressed Ceramic Structures

Author(s): Shanley, F. R.
Corporate Author: Department Of Engineering, University Of California
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1955-01
Report Number: WADC TR 54-75 Part 2
full text available

Heat Transfer and Frictional Effects in Laminar Boundary Layers. Part 4. Universal Series Solutions

Author(s): Tifford, Arthur N.
Corporate Author: Ohio State University Research Foundation
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-08
Report Number: WADC TR 53-288 Part 4
full text available

Evaluation Of Forgings Of Inco And TM-2 Steels At High-Strength Levels

Author(s): Matter, F. A.
Corporate Author: Cleveland Pneumatic Tool Company
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-587
full text available

Preferred Orientation And Deformation In Titaniumand Titanium Alloys

Author(s): McHargue, Carl J.
Corporate Author: University Of Kentucky
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-12
Report Number: WADC TR 54-343
full text available