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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16 reports

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 1. Summary of Technical Work

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 1
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 3. Modal Parameter Estimation

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 3
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 4. System Modeling Techniques

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 4
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 5. Universal File Formats

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 5
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 6. Software User's Guide

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 6
full text unavailable

Information Systems for Space and Earth Science


Corporate Author: Information Systems Office
Date of Publication: 1987-01-01
full text by request

Nonlinear Flying Quality Parameters Based on Dynamic Inversion

Author(s): Morton, B. G.
Corporate Author: Honeywell
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-10-30
Report Number: AFWAL TR 87-3079
full text available

Durability of Continuous Fiber Reinforced Metal Matrix Composites

Author(s): Harmon, D. M.
Corporate Author: McDonnell Aircraft Company and Purdue University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-10-01
Report Number: AFWAL-TR-87-3060
full text by request

Kinetic Mechanisms for Ionization and Afterburning Suppression

Author(s): Weaver, D. P.
Corporate Author: Air Force Astronautics Laboratory
Laboratory: Air Force Astronautics Laboratory
Date of Publication: 1987-11-01
Report Number: AFAL TR 87-49
full text by request

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 2. Measurement Techniques for Experimental Modal Analysis

Author(s): Allenmang, Randall J.
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 2
full text unavailable

Elevated Temperature Crack Growth Studies of Advanced Titanium Aluminides

Author(s): Venkataraman, Srivathsan
Corporate Author: Systran Corporation
Laboratory: Materials Laboratory
Date of Publication: 1987-09-01
Report Number: AFWAL-TR-87-4103
full text by request

Traction Model Development

Author(s): McCool, J. I.
Corporate Author: MRC Bearings-SFK Aerospace
Date of Publication: 1987-09-01
Report Number: AFWAL TR 87-4079
full text by request

Modification of Lubricant Traction Measuring Device

Author(s): Sharma, Shashi K.
Corporate Author: Universal Energy System, Inc.
Date of Publication: 1987-01-01
Report Number: AFWAL TR 86-4031
full text by request

Engine Component Retirement for Cause: Volume I - Executive Summary

Author(s): Harris, John A., Jr.
Corporate Author: United Technologies Corporation
Laboratory: Materials Laboratory
Date of Publication: 1987-08
Report Number: AFWAL-TR-87-4069 Volume I
full text by request

Wind Tunnel Tests of Elliptical Missile Body Configurations at Mach Numbers 0.4 to 0.5

Author(s): Shereda, Donald E.
Corporate Author: High Speed Aero Performance Branch, Aeromechanics Division
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3088
full text by request

An Investigation of Wing Lift Augmentation with Spanwise Tip Blowing

Author(s): Mendenhall, Michael R.
Corporate Author: Nielsen Engineering & Research, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-04-22
Report Number: AFWAL TR 86-3112
full text available