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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96 reports

Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part I. General Applications.

Author(s): Olsen, James J.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Date of Publication: 1969-02
Report Number: AFFDL TR 67-104 Part 1
full text available

Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part II. Application to the AGARD Planforms.

Author(s): Olsen,James J.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Date of Publication: 1969-02
Report Number: AFFDL TR 67-104 Part 2
full text available

Investigation Of The High Pressure Electrodeless Arc In Air

Author(s): Hollister, Donald D.
Corporate Author: Philco-Ford Corp Newport Beach Calif Aeronutronic Div
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1969-02
Report Number: AFFDL TR 68-160
full text available

Parametric Study Of Tsai's Strength Criteria For Filamentary Composites.

Author(s): Sandhu, R. S.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-05
Report Number: AFFDL TR 68-168
full text available

Addresses


Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1-13
full text available

Electroencephalographic and Behavioral Studies of Monomethylhydrazine Toxicity in the Cat

Author(s): Sterman, M. B.
Corporate Author: University of Califronia, Los Angeles
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-06
Report Number: AMRL TR 69-3
full text available

F-105F Transonic Buffet Study and Effect of Maneuvering Flaps

Author(s): Margolin, Milton
Corporate Author: Fairchild Hiller Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-07
Report Number: AFFDL TR 69-37
full text available

Wind Tunnel Tests of a Free-Wing Tilt-Propeller V/STOL Airplane Model

Author(s): Strand, T.
Corporate Author: Air Vehicle Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-10
Report Number: AFFDL TR 69-80
full text available

Propulsion System Integration and Test Program (Steady State). Part II. Shared Exit Ejector Nozzle Static Tests

Author(s): Alfano, David L.
Corporate Author: North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1969-06
Report Number: AFAPL TR 69-44 Part 02
full text available

Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions Part II. Volume I: Facilities and Techniques Employed for Characterization of Candidate Materials

Author(s): Kaufman, Larry
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-84 Part 2 Volume 1
full text available

Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part VI - The Phase Equilibria in the Metal-Rich Region of the Hafnium-Tantalum-Nitrogen System

Author(s): Booker, P. H.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-117 Part 6
full text available

Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part IV - The Effect of Molybdenum and Tungsten on the Subcarbide Solutions in the Vanadium-Tantalum-Carbon and Niobium-Tantalum-Carbon Systems

Author(s): Brukl, C. E.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-08
Report Number: AFML TR 69-117 Part 4
full text available

Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part II - Effect of Rhenium and Aluminum Additions on the Metal-Rich Equilibria in the Titanium-Molybdenum-Carbon and Titanium-Niobium-Carbon Systems

Author(s): Brukl, C. E.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-08
Report Number: AFML TR 69-117 Part 2
full text available

Studies in the Methodology of Weapons Systems Effectiveness Analysis - Using the Techniques of Simulation, Optimization and Statistics - Phase II: Volume III.

Author(s): Julich, Paul M.
Corporate Author: Department of Electrical Engineering, Louisiana State University
Laboratory: Air Force Armament Laboratory
Date of Publication: 1969-12
Report Number: AFATL-TR-69-156 Volume 3
full text available

Development and Experimental Verification of a Computer Program for Predicting Temperature Distribution and Heat Transfer Through Coated and Uncoated, Single or Multi-glaze Window Systems

Author(s): Korb, Gary M.
Corporate Author: Midwest Research Institute
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-04
Report Number: AFFDL TR 69-28
full text available

VTOL Handling Qualities Criteria Study Through Moving-Base Simulation

Author(s): McCormick, R. L.
Corporate Author: Cornell Aeronautical Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-10
Report Number: AFFDL TR 69-27
full text available

Scratch Strain Gage Evaluation

Author(s): Haglage, T. L.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-07
Report Number: AFFDL TR 69-25
full text available

Membrane Elements for Polygonal Cylindrical Reinforced by Rings and Stiffeners

Author(s): Beckers, P.
Corporate Author: Laboratoire De Techniques Aeronatiques et Spatiales, Universite De Liege
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-02
Report Number: AFFDL TR 69-19
full text available

Chemical Vapor Deposition (CVD) Barrel Coating for Refractory Fasteners

Author(s): Wakefield, Gene F.
Corporate Author: Texas Instruments, Incorporated
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-316
full text available

The Compatibilities of Boron and Germanium

Author(s): Bidwell, Lawrence R.
Corporate Author: Air Force Materials Laboratory
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-10
Report Number: AFML TR 69-258
full text available

Fracture Toughness, Fatigue and Corrosion Characteristics of X7080-T7E41 and 7178-T651 Plate and 7075-T6510, 7075-T73510, X7080-T7E42, and 7178-T6510 Extruded Shapes.

Author(s): Kaufman, J. G.
Corporate Author: Aluminum Company of America
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-11
Report Number: AFML TR 69-255
full text available

Manufacturing Methods for Aircraft Tires by Filament-Winding Techniques. Part I.

Author(s): Sanger, Merle J.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-08
Report Number: AFML TR 69-226
full text available

Reinforced Thermoplastics For Making An Expandable, Rigidizable Wing Tip Tank

Author(s): Salyer, I. O.
Corporate Author: Monsanto Research Corporation
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-212
full text available

Design Allowables for Titanium Alloys

Author(s): Martin, Gardner R.
Corporate Author: North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-06
Report Number: AFML TR 69-161
full text available

Analytical Approach to Composite Behavior

Author(s): Ebert, L. J.
Corporate Author: Case Western Reserve Univ Cleveland OH Dept Of Metallurgy
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-06
Report Number: AFML TR 69-129
full text available

Stress Waves in a Laminated Medium Generated by Transverse Forces

Author(s): Voelker, Leonard E.
Corporate Author: Northwestern University
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-08
Report Number: AFML TR 69-120
full text available

Compatibility of Tankage Materials with Liquid Propellants

Author(s): Tiffany, C. F.
Corporate Author: Boeing Company
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-05
Report Number: AFML TR 69-99
full text available

Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions. Part 2. Volume 3. Facilities and Techniques Employed for Hot Gas/Cold Wall Tests

Author(s): Kaufman, Larry
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-84 Part 2 Volume 3
full text available

Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions Part 2. Volume 2: Facilities and Techniques Employed for Cold Gas/Hot Wall Tests

Author(s): Kaufman, Larry
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-12
Report Number: AFML TR 69-84 Part 2 Volume 2
full text available

Dynamic Behavior of Metals Under Tensile Impact. Part I. Elevated Temperature Tests.

Author(s): Schultz, Albert B.
Corporate Author: Illinois Univ At Chicago Circle Dept Of Materials Engineering
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-04
Report Number: AFML TR 69-76 Part 1
full text available

Development Of A Flexible Magnetic Pressure Seal

Author(s): Olson, M. W.
Corporate Author: Uniroyal Inc Wayne N J Research Center
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-02
Report Number: AMRL TR 69-1
full text available

Research and Development of an Integrated Servo Actuator Package for Fighter Aircraft.

Author(s): Koch, Werner G.
Corporate Author: LTV Electrosystems Inc Arlington TX
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-11
Report Number: AFFDL TR 69-109
full text available

Analysis Of Shallow Shells By The Method Of Point Matching

Author(s): Leissa, Arthur W.
Corporate Author: Ohio State Univ Research Foundation Columbus
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-08
Report Number: AFFDL TR 69-71
full text available

Some New Concepts in Oscillatory Lifting Surface Theory.

Author(s): Houbolt, John C.
Corporate Author: Aeronautical Research Associates Of Princeton Inc NJ
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-06
Report Number: AFFDL TR 69-2
full text available

Investigation of Constraints in Thermal Similitude. Volume II.

Author(s): Miller, Paul L.
Corporate Author: Kansas State University Department of Mechanical Engineering
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 69-91 Volume 2
full text available

Investigation of Constraints in Thermal Similitude, Volume 1.

Author(s): Miller, Paul L.
Corporate Author: Kansas State University Department of Mechanical Eningeering
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 69-91 Volume 1
full text available

Water Reclamation by Reverse Osmosis

Author(s): Fossum, John H.
Corporate Author: Melpar, Inc.
Laboratory: Aerospace Medical Research Laboratories
Date of Publication: 1969-05
Report Number: AMRL TR 68-190
full text available

Compound Net Model of the Cerebral Cortex

Author(s): Harth, E. M.
Corporate Author: Syracuse University
Laboratory: Aerospace Medical Research Laboratories
Date of Publication: 1969-06
Report Number: AMRL TR 68-189
full text available

Bacteria Sensor for Reprocessed Water - Microbiological Research, Design, and Fabrication

Author(s): Geating, John A.
Corporate Author: General Electric Company
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-02
Report Number: AMRL TR 68-173
full text available

An Experimental Investigation and System Design for Humidity and Carbon Dioxide Level Control Using Thermal Radiation

Author(s): Maulbetsch, John S.
Corporate Author: Dynatech Corporation
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-04
Report Number: AMRL TR 68-174
full text available

Evaluation of the Use of Commercially Available Detectors for Hydrazine and Nitrogen Dioxide as Colorimetric Dosimeters

Author(s): Rakowski, Robert F.
Corporate Author: Aerospace Medical Research Laboratory
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-02
Report Number: AMRL TR 68-163
full text available

The Acute Inhalation Toxicity of Monomethylhydrazine Vapor

Author(s): Haun, C. C.
Corporate Author: SysteMed Corporation
Laboratory: Aerospace Medical Research Laboratory
Date of Publication: 1969-04
Report Number: AMRL TR 68-169
full text available

Subconvulsive Effects of Monomethylhydrazine on Runway Performance in the Cat

Author(s): Sterman, M. B.
Corporate Author: University of Califronia, Los Angeles
Laboratory: Aerospace Medical Rsearch Laboratory
Date of Publication: 1969-06
Report Number: AMRL TR 68-183
full text available

Progress Report on Discrete-Element Elastic and Elastic-Plastic Analyses of Shells of Revolution Subjected to Axisymmetric and Asymmetric Loading

Author(s): Wimer, Emmett A.,
Corporate Author: Massachusetts Institute of Technology
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1341-1453
full text available

Analysis of the Elastic-Plastic Problems by the Matrix Displacement Method

Author(s): Yamada, Y.
Corporate Author: University of Tokyo; Mitsubishi Atomic Pwer Industries, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1271-1299
full text available

Analysis of Tension Structures

Author(s): Bogner, F. K.,
Corporate Author: Bell Telephone Laboratories, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1253-1270
full text available

An Approximate Analysis of Thin Plates

Author(s): Murray, D. W.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1207-1230
full text available

Hydroelastic of Axisymmetric Systems by a Finite Element Method

Author(s): Guyan, R. J.
Corporate Author: North American Rockwell Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1165-1203
full text available

The Heat Conduction and Thermal Stress Analysis by the Finite Element Method

Author(s): Fujino, T.
Corporate Author: Mitsubishi Heavy Industries, Ltd.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1121-1163
full text available

Analysis of General Coupled Thermoelasticity Problems by the Finite Element Method

Author(s): Oden, J. T.
Corporate Author: Research Institute, University of Alabama, Huntsville
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report Number: AFFDL TR 68-150 p. 1091-1120
full text available