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

8 reports

Active Control Synthesis for Flexible Vehicles: Volume I. KONPACT Theoretical Description

Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 7/1/1976
Report Number: AFFDL TR 75-146 Volume 1
full text available

Active Control Synthesis for Flexible Vehicles: Volume II. KONPACT Program Listing

Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 7/1/1976
Report Number: AFFDL TR 75-146 Volume 2
full text available

Active Control Synthesis for Flexible Vehicles: Volume III. KONPACT User's Manual

Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Date of Publication: 7/1/1976
Report Number: AFFDL TR 75-146 Volume 3
full text available

Vuilleumier Cooler Wear Rate Test Program

Author(s): T. Ohara; K. G. Moore; M. N. Gardos
Corporate Author: Hughes Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 12/1/1976
Report Number: AFFDL TR 76-135
full text available

A Laboratory Investigation into Flight Perturbations During Steep Descents of V/STOL Aircraft

Author(s): L. D. Reid; B. Etkin; H. W. Teunissen; P. C. Hughes
Corporate Author: University of Toronto Institute for Aerospace Studies
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 8/1/1976
Report Number: AFFDL TR 76-84
full text available

Direct Side Force Control Criteria for Dive Bombing: Volume I - Summary

Author(s): Robert V. Brulle; William A. Moran; Richard G. Marsh
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 9/1/1976
Report Number: AFFDL TR 76-78 Volume 1
full text available

An Investigation of Separated Flow About a Hemisphere-Cylinder at 0- to 19-Deg Incidence in the Mach Number Range from 0.6 to 1.5

Author(s): T. Hsieh
Corporate Author: ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 11/1/1976
Report Number: AEDC TR 76-112
full text by request

Space Shuttle


Corporate Author: National Aeronautics and Space Administration
Date of Publication: 1/1/1976
Report Number: NASA SP-407
full text available