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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9 reports

Altimeter Display Study Part I. Summary and Review of Data Requirements

Author(s): W. G. Matheny
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-621 Part 1
full text by request

Altimeter Display Study Part II. Handbook for Static Testing of Altimeters

Author(s): C. B. Elam; W. G. Matheny; D. A. Schum
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-622 Part 2
full text by request

Altimeter Display Study Part III. Summary of Experimental Testing

Author(s): C. B. Elam; W. G. Matheny; D. A. Schum
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-623 Part 3
full text by request

The Effect of Surface Perturbations on the Pressure Distributions About Blunt Two-Dimensional Bodies at High Mach Numbers

Author(s): Coleman duP. Donaldson, Roger D. Sullivan and Wallace D. Hayes
Corporate Author: Aeronautical Research Associates of Princeton, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: FDL TDR 64-17
full text by request

Empirical Correlation of Excitation Environment and Structural Parameters with Flight Vehicle Vibration Response

Author(s): R. W. White; D. J. Bozich; K. M. Eldred
Corporate Author: Northrup Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report Number: AFFDL TR 64-160
full text by request

Extension of Linear Constant-Coefficient Analysis Methods to Time-Varying Systems

Author(s): Walter A. Johnson; Duane T. McRuer; Anil V. Phatak
Corporate Author: Systems Technology, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: RTD TDR 63-4178
full text by request

Digital Adaptive Flight Control System Phase II

Author(s): Dr. R. E. Andeen and P. P. Shipley
Corporate Author: Sperry Phoenix Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-854
full text by request

Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration

Author(s): Kaufman,Louis G., II
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-02
Report Number: RTD TDR 63-4179 Part 1
full text by request

Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures

Author(s): W. H. Roberts and P. E. Finwall
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: ASD TDR 62-801 Supplement I
full text by request