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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12 reports

Fighter Technology Demonstrator Precursor Analysis and Test: Volume I. Baseline Development and Technology Identification

Author(s): None Given
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report Number: AFFDL TR 73-112 Volume 1
full text by request

Design Methods for Specifying Handling Qualities for Control Configured Vehicles: Volume I Technical Discussion

Author(s): Brulle, R. V.
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report Number: AFFDL-TR-73-142 Volume I
full text by request

STOL Tactical Aircraft Investigation Volume I Configuration Definition: Medium STOL Transport with Vectored Thrust/Mechanical Flaps

Author(s): Carroll, Richard H.
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report Number: AFFDL TR 73-19 Volume 1
full text by request

Ejector Blown Lift/Cruise Flap Wind Tunnel Investigation

Author(s): Clark, Rodney L.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report Number: AFFDL TR 73-132
full text by request

STOL Tactical Aircraft Investigation Volume V, Part I Flight Control Technology: System Analysis and Trade Studies for a Medium STOL Transport with Vectored Thrust/Mechanical Flaps

Author(s): Crandall, Kenneth J.
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report Number: AFFDL TR 73-19 Volume 5 Part 1
full text by request

Development of an Empirically Based Computer Program to Predict the Aerodynamic Characteristics of Aircraft Volume II. Program User Guide

Author(s): Schemensky, Roy T.
Corporate Author: General Dynamics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report Number: AFFDL TR 73-144 Volume II
full text by request

Format-Fortran Matrix Abstraction Technique: Volume II - Supplement IV: Description of Digital Computer Program-Extended

Author(s): Chahinian, L.
Corporate Author: Doulgas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report Number: AFFDL TR 66-207 Volume II Supplement IV
full text by request

STOL Tactical Aircraft Investigation - Externally Blown Flap Volume I Configuration Definition

Author(s): Owens, H. G.
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report Number: AFFDL TR 73-20 Volume 1
full text by request

STOL Tactical Aircraft Investigation: Volume I Configuration Definition

Author(s): Herbert, J.
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report Number: AFFDL TR 73-21 Volume 1
full text by request

STOL Tactical Aircraft Investigation: Volume II Design Compendium

Author(s): Levinsky, E. S.
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-05
Report Number: AFFDL TR 73-21 Volume 2
full text by request

Format-Fortran Matrix Abstraction Technique: Volume V Supplement II: Engineering User and Technical Report-Extended

Author(s): Pickard, J.
Corporate Author: Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report Number: AFFDL TR 66-207 Volume V Supplement II
full text by request

STOL Tactical Aircraft Investigation - Externally Blown Flap Volume IV Analysis of Wind Tunnel Data

Author(s): Papp, P. P.
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report Number: AFFDL TR 73-20 Volume 4
full text by request