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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8 reports

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): Louis G. Kaufman 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

Six-Degree-of-Freedom Flight Path Study Generalized Computer Program: Part II, Volume 2 - User's Manual for Part I, Volume 2

Author(s): J. L. Harris, J. A. Shilling and R. F. Vorwald
Corporate Author: McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-1 Part 2 Volume 2
full text by request

Development of an Advanced Digital Adaptive Flight Control System

Author(s): J. Zaborszky, W. J. Luedde, R. L. Berger, J. B. Berger and M. A. Madonna
Corporate Author: McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report Number: FDL TDR 64-115
full text by request

Thermal Response in Sandwich Panels

Author(s): P. Kendall
Corporate Author: Martin Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-135
full text by request

Approximate Methods of Simulating Random Noise with Pure Tone Sources

Author(s): C. C. Thiel
Corporate Author: General Technology Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report Number: FDL TDR 64-131
full text by request

Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Coporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-07
Report Number: ASD TDR 63-679 Part 4
full text by request

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

Author(s): Kaufman,Louis G., II
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report Number: RTD TDR 63-4179 Part 2
full text by request

Design of Linear Flight Control Systems Using Optimal Control Theory

Author(s): E. G. Rynaski, P. A. Reynolds and W. H. Shed
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: ASD TDR 63-376
full text by request