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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13 reports

Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls

Author(s): L. R. Fenzel; K. C. Nichol; L. R. Wood
Corporate Author: General Electric Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report Number: ASD TDR 62-76
full text unavailable

Investigation of Hypersonic Flow Separation and its Effects on Aerodynamic Control Characteristics

Author(s): Douglas E. Abbott; Maurice Holt; Jack N. Nielsen
Corporate Author: Itek Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-11
Report Number: ASD TDR 62-963
full text unavailable

Hypersonic Flow Theories for Predicting Pressures on Blunt Two-Dimensional and on Conical Shapes

Author(s): Richard A. Scheuing; Robert E. Melnik; John W. Brook; Wallace D. Hayes; Coleman duP. Donaldson; Rofer D. Sullivan
Corporate Author: Grumman Aircraft Engineering Corporation; Aeronautical Research Associates of Princeton
Laboratory: Flight Control Laboratory
Date of Publication: 1962-06
Report Number: ASD TDR 62-167
full text unavailable

Design Techniques and Laboratory Development of an Electrical Primary Flight control System

Author(s): V. C. Sethre; R. E. Schenbeck; R. L. Kerber; J. A. Rassi; R. L. Fowler
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report Number: ASD TDR 62-46
full text unavailable

An Investigation of Magnetohydrodynamic Principles Applicable to Flight Control

Author(s): William B. Ericson; Algirdas Maciulaitis; Frank A. Spagnolo; Albert L. Loeffler; Richarde A. Scheuing; Harold B. Hopkins
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-649
full text unavailable

Study of Electrically Produced Strain for Control Purposes

Author(s): None Given
Corporate Author: Bendix Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-621
full text unavailable

Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8

Author(s): Harold R. Mead; Frank Koch
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report Number: ASD TR 61-60 Part 2
full text unavailable

Automatic Landing System Study: Part II. Results of Ground Equipment and Data Transmission Studies

Author(s): R. Wilkie; C. Smearmon; R. Cope
Corporate Author: Bendix Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-114 Part 2
full text unavailable

Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume I Elastic Response Determinations for Severely Heated Wings

Author(s): Richard H. Gallagher: Rolland D. Huff
Corporate Author: Bell Aerosystems Co.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-08
Report Number: ASD TR 61-287 Part 2 Volume 1
full text unavailable

Basic Research and Development in Fluid Power Control

Author(s): None Given
Corporate Author: Massachusetts Institute of Technology
Laboratory: Flight Control Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-349
full text unavailable

Study and Development of an Electric Side Stick Controller for Aerospace Vehicles

Author(s): Harry C. Graves; A. James Bailey; David L. Mellen
Corporate Author: Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report Number: ASD TR 61-603
full text unavailable

Hydraulic Servo Control Valves - Part 8 Valve Performance Evaluation Investigation Of Oil Contamination Effects, And Nuclear Radiation Effects Testing

Author(s): Kinney, Wayne L.; Dick, George H.
Corporate Author: Cook Technological Center
Laboratory: Flight Control Laboratory
Date of Publication: 1962-10
Report Number: WADC TR 55-29 Part 8
full text unavailable

The Effects of Body Camber on Body Pressure Distributions and Wing Forces for Mach Numbers from 2.0 to 7.6: Part I: Experimental Data

Author(s): F. H. Durgin & W. C. Noz, Jr.
Corporate Author: Massachusetts Institute of Technology Naval Supersonic Facility
Laboratory: Flight Control Laboratory
Report Number: ASD TR 61-295 Part I
full text unavailable