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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138 reports

Research on Transition Metal-Carbon Chemistry

Author(s): Wilkinson, Geoffrey
Corporate Author: Imperial College of Science and Technology
Date of Publication: 1962-07
Report Number: ASD TR 61-359
full text unavailable

Synthesis And Reactions Of Substituted Ethers, Amino-Derivatives, Thioethers And Disulfides Of S-Triazines

Author(s): Ehlers, Gerhard F.
Corporate Author: Aeronautical Systems Division
Laboratory: Aeronautical Systems Division
Date of Publication: 1962-12
Report Number: ASD TDR 62-863
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Regenerative Fuel Cell System

Author(s): Schwartz, H. J.
Corporate Author: TRW, Inc.
Date of Publication: 1962-04
Report Number: ASD TDR 62-18
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Optical Methods Of Measuring Plasma Jet Temperatures. Part III: Measurement By Photoelectric Pyrometry

Author(s): Hottel, H. C.
Corporate Author: Massachusetts Institute Of Technology
Date of Publication: 1962-02
Report Number: WADD TR 60-676 Part 2
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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): Mead, Harold R.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report Number: ASD TR 61-60 Part 2
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Study and Development of an Electric Side Stick Controller for Aerospace Vehicles

Author(s): Graves, Harry C.
Corporate Author: Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report Number: ASD TR 61-603
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Deformation and Ductile Fractures of Metals in Torsion and Tension

Author(s): Polakowski, N. H.
Corporate Author: Illinois Inst. of Tech. Dept. of Metallurgical Engineering
Date of Publication: 1962-02
Report Number: AFOSR-2276
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Research on Inorganic Polymer Systems

Author(s): Steinberg, Howard
Corporate Author: United States Borax Research Corporation
Date of Publication: 1962-11-30
Report Number: ASD TDR 62-251 Part 2
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A Study of Manual and Automatic Control Systems for the Terminal Phase of Orbital Rendezvous Part I. Basic Guidance and Control Information

Author(s): Thomspon, Hugh B.
Corporate Author: Systems Technology, Inc.
Laboratory: Directorate of Advanced Systems Planning
Date of Publication: 1962-06
Report Number: ASD TR 61-344
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Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles

Author(s): Henson, J. R.
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report Number: AEDC TDR 62-7
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Adverse Weather Tests of the H-43B Helicopter

Author(s): Moore, James R.
Corporate Author: Directorate of Flight Test
Laboratory: Directorate of Flight Test
Date of Publication: 1962-11
Report Number: ASD TDR 62-454
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Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls

Author(s): Fenzel, L. R.
Corporate Author: General Electric Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report Number: ASD TDR 62-76
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Investigation of Intermetallic Compounds for Very High Temperature Applications

Author(s): Booker, Jonathan
Corporate Author: Brush Beryllium Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-07
Report Number: WADD TR 60-889 Part II
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Mechanism of Wear of Nonmetallic Materials

Author(s): Riesz, C. H.
Corporate Author: Armour Research Foundation
Date of Publication: 1962-06
Report Number: WADC TR 59-316 Part 4
AD Number: AD0284551
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Molecular Structure and Physical Behavior of Polymers

Author(s): Morton, M.
Corporate Author: University of Akron
Date of Publication: 1962-05
Report Number: ASD TR 61-16 Part 2
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Practical Aspects of Aerothermoelastic Modelling

Author(s): Schlessinger, M.
Corporate Author: Flight Sciences Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-705
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New Approaches to Flight Vehicle Structural Vibration Analysis and Control

Author(s): Heck, Manfred A.
Corporate Author: Bolt, Beranek & Newman, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-237
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Calibration Tests of a Litton Conical Air Data Probe at Mach Numbers of 2 to 8

Author(s): Mallard, Scott R.
Corporate Author: ARO, Inc.
Date of Publication: 1962-10
Report Number: AEDC TDR 62-186
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Studies of Reactor Containment Structures

Author(s): Weil, N. A.
Corporate Author: Armour Research Foundation
Date of Publication: 1962-09-14
AD Number:
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Development of 2400 F Forging Die System

Author(s): Nudelman, H. B.
Corporate Author: Armour Research Foundation
Date of Publication: 1962-10
Report Number: ASD TR 7-886 Volume 6
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Effect of a Disperse Phase on the Ductile Brittle Transition of Body Centered Cubic Metals

Author(s): Evans, P. R. V.
Corporate Author: Armour Research Foundation
Report Number: ARL 62-301
AD Number:
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Design And Reliability Study For A-C Generators And Controls

Author(s): Mueller, P. M.
Corporate Author: Jack & Heintz, Inc.
Laboratory: Flight Accessories Laboratory
Date of Publication: 1962-08
Report Number: WADD TR 61-85
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Literature Survey and Bibliography. Ultrahighpressure Effects on Organic, Inorganic, and Semi-Organic Materials

Author(s): Mayer, R. A.
Corporate Author: Battelle Memorial Institute
Date of Publication: 1962-01
Report Number: ASD TDR 62-72
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Uniform Heating Effects on the Response of a High Speed Vehical to Discrete and Continuous Gusts

Author(s): Peboulet, R. P.
Corporate Author: General Dynamics
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-328
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Research On Vaccum Evaporated And Cathode Sputtered Thin Films

Author(s): Belster, R. B.
Corporate Author: Georgia Institute Of Technology, Engineering Experiment Station
Date of Publication: 1962-02
Report Number: WADD TR 60-381
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A Study of Manual and Automatic Control Systems for the Terminal Phase of Orbital Rendezvous

Author(s): Stapleford, Robert L.
Corporate Author: Systems Technology, Inc.
Laboratory: Directorate of Advanced Systems Plannin
Date of Publication: 1962-06
Report Number: ASD TDR 62-82
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume I Elastic Response Determinations for Severely Heated Wings

Author(s): Gallagher, Richard H.
Corporate Author: Bell Aerosystems Co.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-08
Report Number: ASD TR 61-287 Part 2 Volume 1
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Design Techniques and Laboratory Development of an Electrical Primary Flight control System

Author(s): Sethre, V. C.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report Number: ASD TDR 62-46
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An Engineering Evaluation of Methods for the Prediction of Fatigue Life in Airframe Structures

Author(s): Crichlow, W. J.
Corporate Author: Lockheed Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: ASD TR 61-434
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Research On Protection Of High Temperature Glass Fibers Against Flexing And Abrasion

Author(s): Edmunds, W. M.
Corporate Author: Owens-Corning Fiberglas Corporation
Date of Publication: 1962-11
Report Number: ASD TDR 62-935
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Investigation of Glass Fiber Strength Enhancement through Bundle Drawing

Author(s): Weil, N. A.
Corporate Author: Armour Research Foundation
Date of Publication: 1962-05
AD Number: AD0287404
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Study to Determin Skin-Friction Drag in Hypersonic Low-Density Flow: Vlume I: Summary Analysis

Author(s): Francis, W. Leon
Corporate Author: Lockheed-California Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-433 Volume 1
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An Investigation of Magnetohydrodynamic Principles Applicable to Flight Control

Author(s): Ericson, William B.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-649
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Standardization Of Thermal Emittance Measurements. Part III. Normal Spectral Emittance, 800-1400 K

Author(s): Harrison, William N.
Corporate Author: National Bureau of Standards
Date of Publication: 1962-03
Report Number: WADC TR 59-510 Part 3
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Feasibility of Neutron Diffraction Studies in High Pressure

Author(s): Wolf, G. H.
Corporate Author: Illinois Inst. of Tech. Armour Research Foundation
Date of Publication: 1962-05-10
AD Number: AD0277846
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Determination of A3D Angle of Attack Setting for Carrier Approach

Author(s): Smith, A. A., Jr.
Corporate Author: Naval Air Test Center
Date of Publication: 1962-08-31
AD Number: AD0284861
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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): Durgin, F. H.
Corporate Author: Massachusetts Institute of Technology Naval Supersonic Facility
Laboratory: Flight Control Laboratory
Report Number: ASD TR 61-295 Part I
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Liner for Extrusion Billet Containers

Author(s): Spachner, S. A.
Corporate Author: Armour Research Foundation
Date of Publication: 1962-12-05
Report Number: ASD TDR 7-945 Volume 2
AD Number: AD0295626
full text unavailable