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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57 reports

New Remotely Piloted Vehicle Launch and Recovery Concepts - Computer Program Listings

Author(s): Baumgartner, S. J.
Corporate Author: Boeing Aerospace Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1979-06
Report Number: AFFDL TR 79-3069 Volume II
full text by request

New Concepts in Aircraft Journal Bearings

Author(s): Lynn, W. F.
Corporate Author: Boeing Commercial Airplane Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1978-08
Report Number: AFFDL TR 78-97
full text by request

Human Engineering Support to Air Force Flight Control and Flight Display Integration Program

Author(s): Rabideau, Gerald F.
Corporate Author: The Bunker-Ramo Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-10
Report Number: AFFDL TR 66-157
full text by request

A Theoretical and Experimental Investigation of the Free Piston Cycle

Author(s): Humphrey, Burton G., Jr.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-02
Report Number: AFFDL TR 66-204
full text by request

Laboratory Tests of an Air Cushion Recovery System for the Jindivik Aircraft

Author(s): Vaughan, John C., III
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1974-04
Report Number: AFFDL TR 74-64
full text by request

Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G., II
Corporate Author: Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report Number: RTD TDR 63-4239
full text by request

Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics

Author(s): Kaufman, Louis G., II
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-10
Report Number: RTD TDR 63-4044 Part 1
full text by request