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Preparation And Investigation Of High-Strength Wires
Report Number: AFML TR 67-35
Author(s): Pfouts, W. R.; Moazed, K. L.
Corporate Author: Ohio State University Research Foundation
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 50
Contract: AF 33(615)-1717
Project: 7353
Task: 735301
AD Number: AD0822595
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The Effect Of Testing System Stiffness On Fracture Behavior Of Sheet Specimens
Report Number: AFML TR 67-37
Author(s): Weiss, V.; Grewal, K.; Rosenberg, W.; Lin, R.
Corporate Author: Syracuse University
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 100
Contract: AF 33(615)-1602
Project: 7351
Task: 735106
AD Number: AD0821943
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Stress-Strain Response Of Fabrics Under Two-Dimensional Loading
Report Number: AFML TR 67-44
Author(s): Freeston, W. Denney, Jr.; Platt, Milton M.; Schoppee, Meredith M.
Corporate Author: Fabric Research Laboratories, Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 7/1/1967
Pages: 81
Project: 7320
Task: 732002
AD Number: AD0658870
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Description Of A Continuing Program On Tables Of Thermophysical Properties Of Materials
Report Number: AFML TR 67-81
Author(s): Ho, C. Y.
Corporate Author: Purdue University
Laboratory: Air Force Materials Laboratory
Publication Date: 3/1/1967
Pages: 49
Contract: AF 33(615)-2281
Project: 7381
Task: 738103
AD Number: AD0815784
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Directory Of Graphite Availability. Second Edition.
Report Number: AFML TR 67-113
Author(s): Glasser, Julian; Glasser, William J.
Corporate Author: Chemical and Metallurgical Research, Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 356
Features: + Graph(s) + Table(s)
Contract: AF 33(615)-3430
Project: 7381
Task: 738102
AD Number: AD0821777
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Abstract Text:
This directory was prepared for the purpose of assisting development, application, and design engineers in the rapid identification of graphite materials and sources of supply. This is a revision and updating of the first directory published in 1963 and it is expected that continuing revision, supplements, or new editions will be needed. A total of 262 graphite products, available from 19 suppliers, atre characterized by type, manufacturing methods, analyses, and properties. For each of these products, supplier's availability on grades, sizes and shapes, price, rate or capacity of production, and delivery times are shown. An indexing system allows for the convenient finding of information on suppliers, sizes and shapes, unique characteristics, compositions, and properties.
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Micromechanics Of High Strength, Low Density, Boron Filament Reinforced Aluminum Metallic Composites
Report Number: AFML TR 67-125 Part 2
Author(s): Lenoe, E. M.; Murro, R. P.; Beaumont, S.; Wu, J.
Corporate Author: AVCO Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1967
Pages: 84
Contract: AF 33(615)-3076
Project: 7351
Task: 735107
AD Number: AD0834303
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Investigation of Nondestructive Methods for the Evaluation of Graphite Materials, Part 2.
Report Number: AFML TR 67-128 Part 2
Author(s): Stinebring, R. C.; Schultz, A. W.; Orner, J. W.
Corporate Author: Avco Government Products Group Wilmington Ma Avco Space Systems Div
Laboratory: Air Force Materials Laboratory
Publication Date: 2/1/1969
Pages: 116
Contract: AF 33(615)-3942
Project: 7351
Task: 735109
AD Number: AD0851233
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Research On Boron Filament/Metal Matrix Composite Materials
Report Number: AFML TR 67-140
Author(s): Wolff, Ernest G. Hill, Russell J.
Corporate Author: Avco Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 6/1/1967
Pages: 161
Contract: AF 33(615)-3164
Project: 7351
Task: 735107
AD Number: AD0816439
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Research To Optimize The Filament-Wound Toroidal Tire To Provide Performance To Tests Of Specification Mil-T-5041d At Minimum Weight
Report Number: AFML TR 67-154
Author(s): Salcedo, Frank S.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 6/1/1967
Pages: 76
Features: + Foldout(s)
Contract: AF 33(615)-5024
Project: 7381
Task: 738101
AD Number: AD0818075
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Research on Exploratory Development of Nondestructive Methods for Crack Detection. Part III.
Report Number: AFML TR 67-167 Part 3
Author(s): Schroeer, Rudi M.
Corporate Author: Arvin Systems Inc Dayton OH
Laboratory: Air Force Materials Laboratory
Publication Date: 3/1/1970
Pages: 72
Contract: F33615-69-C-1104
Project: 7351
Task: 735109
AD Number: AD0867801
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Tantalum Alloy Tubing Development Program
Report Number: AFML TR 67-191
Author(s): Turner, Fred S.
Corporate Author: Allegheny Ludlum Steel Corporation Research Center
Laboratory: Air Force Materials Laboratory
Publication Date: 6/1/1967
Pages: 400
Contract: AF 33(657)-11261
AD Number: AD0819050
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Development of Improved Methods of Depositing Iridium Coatings on Graphite.
Report Number: AFML TR 67-195 Part 2
Author(s): Macklin, Buford A.; LaMar, Paul A.
Corporate Author: General Technologies Corp Springfield VA
Laboratory: Air Force Materials Laboratory
Publication Date: 9/1/1968
Pages: 82
Contract: AF 33(615)-3617
Project: 7350
Task: 735002
AD Number: AD0843766
Photo Enhancement: Complete
Abstract Text:
Oxidation protection of graphite by the formation of a pore- and crack-free iridium coating has been accomplished. A multiplicity of chemical vapor deposition, fused-salt, and aquesous electrodeposition methods were evaluated for the preparation of iridium coatings. While it was possible to deposit coatings 1 to 3 mils in thickness in one processing step, such thick deposits tended to develop trees and nodules. Thick coating (3 to 8 mils) were deposited on samples provided to AFML in multiple depositions of 0.5 mils each. The entrapment of solutions from aqeuous electrodeposition caused cracking in the graphite and precluded its use for depositing iridium coatings. Efforts to form an iridium-rhenium alloy by fused-salt electrolysis and aqueous electrodeposition from electrolytes containing both elements were not successful. Only iridium was obtained from fused salts and the deposits from the aqeuous electrolytes were not homogeneous. Likewise, effortd to increase the emittance of iridium by inclusion of either ThO2 or HfO2 in iridium from fused salts were not successful. A method of nondestructive testing of the oxidation resistance of the iridium by a gas-chromatographic method showed promise as an evaluation technique.
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Mechanisms Of Fatigue Hardening In Copper Single Crystals
Report Number: AFML TR 67-203
Author(s): Hancock, J. B.; Grosskreutz, J. C.
Corporate Author: Midwest Research Institute
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 58
Contract: AF 33(657)-3987
Project: 7353
Task: 735301
AD Number: AD0821085
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Process Variables In Metal Extrusion, Part I: Liner Friction During Extrusion
Report Number: AFML TR 67-242 Part 1
Author(s): Carnahan, D. R.; DePierre, V.
Corporate Author: Westinghouse Astronuclear Lab Pittsburgh PA
Laboratory: Air Force Materials Laboratory
Publication Date: 7/31/1967
Pages: 28
Contract: AF 33(615)-5817
Project: None Given
Task: None Given
AD Number: AD0827977
Photo Enhancement: Complete
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Development Of An Alignment And Measuring System For Large Aerospace Vehicles. Volume I.
Report Number: AFML TR 67-255 Volume 1
Author(s): Steinhacker, Mark
Corporate Author: Kollsman Instrument Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/967
Pages: 154
Features: + Foldout(s)
Contract: AF 33(657)-11724
Project: 8-125
AD Number: AD0823179
Photo Enhancement: Incomplete
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Development Of An Alignment And Measuring System For Large Aerospace Vehicles. Volume II.
Report Number: AFML TR 67-255 Volume 2
Author(s): Steinhacker, Mark
Corporate Author: Kollsman Instrument Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 410
Features: + Foldout(s)
Contract: AF 33(657)-11724
Project: 8-125
AD Number: AD0823180
Photo Enhancement: Not Needed
Notes: pagination continued from volume 1
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Evaluation of Welded and Brazed Stainless Steels and Superalloys in a Corrosive Environment
Report Number: AFML TR 67-258
Author(s): O'Connor, J. J.; Vozzella, P. A.
Corporate Author: Pratt And Whitney Aircraft Group East Hartford CT
Laboratory: Air Force Materials Laboratory
Publication Date: 10/1/1968
Pages: 135
Contract: AF 33(615)-5129
Project: 7381
Task: 738107
AD Number: AD0845626
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Compilation Of Tensile And Creep Rupture Data Of Several Al, Mg, Ti, And Steel Alloys, And Ni Superalloys
Report Number: AFML TR 67-259
Author(s): None Given
Corporate Author: Air Force Materials Lab Wright-Patterson AFB OH
Laboratory: Air Force Materials Laboratory
Publication Date: 4/1/1968
Pages: 954
Features: + Map(s) + Table(s)
Contract: AF 33(600)-32008
Project: 7381
Task: 738103
AD Number: AD0834771
Photo Enhancement: Not Needed
Abstract Text:
A program was conducted to determine the feasibility and possible advantage of processing conventional creep data through the use of computer program technology and to make generally available previously unpublished creep data. Computer programs were developed to fit data, make necessary calculations, tabulate results, and plot finished curves ready for design use. Raw creep data on 24 materials conducted over several years were processed and are presented in the normal format of tensile and creep data.
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Development Of A New High-Strength Semiaustenitic Precipitation-Hardenable Stainless Steel.
Report Number: AFML TR 67-286
Author(s): Moll, J. H.; Stasko, W.; Kasak, A.
Corporate Author: Crucible Steel Company of America
Laboratory: Air Force Materials Laboratory
Publication Date: 9/1/1967
Pages: 140
Contract: AF 33(615)-2201
Project: 7351
Task: 735105
AD Number: AD0823235
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Stress Corrosion Susceptibility Of Welded Aluminum Alloys
Report Number: AFML TR 67-291
Author(s): Turley, Richard F.; Avery, Charles H.; Dash, Edward
Corporate Author: Douglas Aircraft Company
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 164
Contract: AF 33(615)-5419
Project: 7381
Task: 738107
AD Number: AD0824852
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Study Of The Hot Corrosion Of Superalloys
Report Number: AFML TR 67-297
Author(s): Walters, J. J.
Corporate Author: Avco Lycoming Div Stratford CT
Laboratory: Air Force Materials Laboratory
Publication Date: 9/1/1967
Pages: 159
Project: 0
Task: 0
AD Number: AD0822779
Photo Enhancement: Complete
Abstract Text:
The effect of operating environment and alloy composition on the nature and extent of oxidation-sulfidation attack was studied with the aid of the Lycoming environmental test rig, which operates at one atmosphere pressure. Sulfidation attack was produced by burning JP-4, JP-4R, and JP-5 fuels (sulfur contents of .02, .16, and .16 weight percent respectively) while ingesting synthetic sea water at controlled rates to yield salt/air ratios of 4ppm and 8ppm. Specimens of 11 nickel base and one cobalt base alloy were subjected to cyclic temperatures, holding at peak temperatures of 1600 F or 1750 F for ten minutes per cycle. The temperature range over which sulfidation occurred and the depth of attack increased with increasing salt-to-air ratios and with time of exposure. Good resistance to attack was generally associated with higher chromium content but high chromium alone did not guarantee good resistance to attack. Microprobe and x-ray investigations indicated that chromium-rich surface oxides provide good resistance to sulfidation and that high aluminum-titanium ratios provide good oxidation resistance.
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Investigation Of Hot Corrosion Of Nickel Base Superalloys Used In Gas Turbine Engines
Report Number: AFML TR 67-306
Author(s): Ryan, Kenneth H.; Hamilton, Paul E.; Kildsig, John R.
Corporate Author: General Motors Corp Indianapolis In Allison Gas Turbine Div
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1967
Pages: 100
Features: + Foldout(s)
Contract: AF 33(615-5211
Project: 7381
AD Number: AD0825297
Photo Enhancement: Incomplete
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Nonsteady-State Thermal Stress Behavior Of Refractory Materials
Report Number: AFML TR 67-315
Author(s): Bohn, Jack R.; King, Kenneth R.; Ernst, Charles H.; Janowski, Kenneth R.
Corporate Author: TRW Systems
Laboratory: Air Force Materials Laboratory
Publication Date: 11/1/1967
Pages: 149
Contract: AF 33(615)-3727
Project: 7381
Task: 738102
AD Number: AD0823487
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Refractory Metal Coatings By The Fused Salt Method
Report Number: AFML TR 67-318
Author(s): Steinman, J. B.; Warnock, R. V.; Root, C. G.; Stetson, A. R.
Corporate Author: Solar Turbines International San Diego CA
Laboratory: Air Force Materials Laboratory
Publication Date: 10/1/1967
Pages: 168
Contract: AF 33(615)-3173
Project: 8-346
AD Number: AD0822043
Photo Enhancement: Incomplete
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Development Of Manufacturing Methods For Producing Pyrolytic Graphite In Various Shapes And Structures
Report Number: AFML TR 67-344
Author(s): Clark, Thomas J.
Corporate Author: General Electric Co Detroit Mi Metallurgical Products Dept
Laboratory: Air Force Materials Laboratory
Publication Date: 11/1/1967
Pages: 612
Features: + Diagram(s) + Drawing(s) + Foldout(s) + Graph(s) + Photo(s) + Table(s)
Contract: AF 33(615)-3136
Project: None Given
Task: None Given
AD Number: AD0824697
Photo Enhancement: Complete
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Evaluation of High-Temperature Resins in Asbestos Fiber Reinforced Laminates
Report Number: AFML TR 67-389
Author(s): M. B. Smith
Corporate Author: Whittaker Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 3/1/1968
Pages: 79
Features: + Foldout(s)
Contract: AF 33(615)-5071
Project: 7381
Task: 738106
AD Number: AD0834698
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