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Silicon Carbide Whisker-Metal Matrix Composites
Report Number: AFML TR 69-7
Author(s): Divecha, Amarnath P.; Lare, Paul J.; Hahn, Henry
Corporate Author: Melpar Falls Church VA
Laboratory: Air Force Materials Laboratory
Publication Date: 5/1/1969
Pages: 92
Features: + Foldout(s)
Contract: F33615-68-C-1064
AD Number: AD0854793
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Fatigue, Creep, and Stress-Rupture Properties of Several Super Alloys
Report Number: AFML TR 69-12
Author(s): Blatherwick, Allan A.; Cers, Austris E.
Corporate Author: Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory: Air Force Materials Laboratory
Publication Date: 1/1/1969
Pages: 161
Contract: F33615-67-C-1527
Project: 7381
Task: 738106
AD Number: AD0850949
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Strengthening of Titanium Alloys by Shock Deformation
Report Number: AFML TR 69-14
Author(s): Greedis, John F.; Koul, M. Kishen
Corporate Author: Massachusetts Institute of Technology
Laboratory: Air Force Materials Laboratory
Publication Date: 2/1/1969
Pages: 19
Contract: AF 33(615)-3866
Project: 7351
AD Number: AD0851481
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Corrosion Cracking of Metallic Materials
Report Number: AFML TR 69-16
Author(s): Fontana, Mars G.
Corporate Author: Ohio State Univ Columbus Dept Of Metallurgical Engineering
Laboratory: Air Force Materials Laboratory
Publication Date: 2/1/1969
Pages: 146
Contract: AF 33(615)-5108
Project: 7312
Task: 731202
AD Number: AD0849870
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Thermally Activated Deformation in Alpha Titanium
Report Number: AFML TR 69-59
Author(s): Gegel, H. L.; Duvall, T.
Corporate Author:
Laboratory: Air Force Materials Laboratory
Publication Date: 4/1/1969
Pages: 68
Contract: Laboratory Research - No Contract
Project: 7353
Task: 735302
AD Number: AD0853530
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Behavior Study of Sapphire Wool Aluminum and Aluminum Alloy Composites
Report Number: AFML TR 69-62
Author(s): Mehan, R. L.; Jakas, R.
Corporate Author: General Electric Co Philadelphia PA Missile And Space Div
Laboratory: Air Force Materials Laboratory
Publication Date: 3/1/1969
Pages: 88
Contract: F33615-67-C-1308
Project: 7351
Task: 735107
AD Number: AD0851936
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Dynamic Behavior of Metals Under Tensile Impact. Part I. Elevated Temperature Tests.
Report Number: AFML TR 69-76 Part 1
Author(s): Schultz, Albert B.
Corporate Author: Illinois Univ At Chicago Circle Dept Of Materials Engineering
Laboratory: Air Force Materials Laboratory
Publication Date: 4/1/1969
Pages: 44
Contract: F33615-67-C-1283
Project: 7351
Task: 735106
AD Number: AD0853260
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Abstract Text:
The mechanical behavior of metals subjected to uniaxial tensile impact at elevated temperatures is reported. Tests were conducted on annealed 1100 aluminum at 200 degrees, 350 degrees, 550 degrees, and 800 degrees F; annealed 2024 aluminum at 200 degrees, 450 degreees, and 600 degrees; and annealed C1010 steel at 430 degrees, 700 degrees, 1050 degrees, and 1400 degrees F. The materials exhibit a wide range of dynamic behavior, including some in which the stress required to produce a given level of strain is siginificantly lowered by dynamic loading. The ratios of the dynamic ultimate stresses to the static are found to range from 0.71 to 6.0.
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Dynamic Behavior of Metals Under Tensile Impact. Part II: Annealed and Cold Worked Materials.
Report Number: AFML TR 69-76 Part 2
Author(s): Schultz, Albert B.
Corporate Author: Illinois Univ At Chicago Circle Dept Of Materials Engineering
Laboratory: Air Force Materials Laboratory
Publication Date: 6/1/1969
Pages: 39
Contract: F33615-67-C-1283
Project: 7351
Task: 735106
AD Number: AD0857984
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A Continuing Systematic Program On Tables Of Thermophysical Properties Of Materials
Report Number: AFML TR 69-79
Author(s): Ho, C. Y.
Corporate Author: Thermophysical And Electronic Properties Information Analysis Center Lafayette IN
Laboratory: Air Force Materials Laboratory
Publication Date: 4/1/1969
Pages: 95
Contract: F33615-68-C-1229
Project: 7381
Task: 738103
AD Number: AD0688969
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Studies of Gas-Solid Interactions Using a Modulated Beam Mass Spectrometer
Report Number: AFML TR 69-80
Author(s): Steele, Warren G.
Corporate Author:
Publication Date: 4/1/1969
Project: 0
Task: 0
AD Number: AD0854382
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Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions Part II. Volume I: Facilities and Techniques Employed for Characterization of Candidate Materials
Report Number: AFML TR 69-84 Part 2 Volume 1
Author(s): Larry Kaufman and Harvey Nesor
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 86
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865317
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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
Report Number: AFML TR 69-84 Part 2 Volume 2
Author(s): Kaufman, Larry; Nesor, Harvey
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 55
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0864968
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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
Report Number: AFML TR 69-84 Part 2 Volume 3
Author(s): Kaufman, Larry; Nesor, Harvey
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 122
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865316
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Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions. Part 3. Volume 1. Experimental Results of Low Velocity Cold Gas/Hot Wall Tests
Report Number: AFML TR 69-84 Part 3 Volume 1
Author(s): Kaufman, Larry; Nesor, Harvey
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 117
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865319
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Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions. Part 3. Volume 2. Experimental Results of High Velocity Cold Gas/Hot Wall Test
Report Number: AFML TR 69-84 Part 3 Volume 2
Author(s): Kaufman, Larry; Nesor, Harvey; Perkins, Roger
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 125
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865323
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Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions. Part 3, Volume 3: Experimental Results of High Velocity Hot Gas/Cold Wall Tests.
Report Number: AFML TR 69-84 Part 3 Volume 3
Author(s): Kaufman, Larry; Nesor, Harvey
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 2/1/1970
Pages: 336
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0867307
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Stability Characterization of Refractory Materials under High Velocity Atmospheric Flight Conditions. Part 4. Volume 1. Theoretical Correlation of Material Performance with Stream Conditions
Report Number: AFML TR 69-84 Part 4 Volume 1
Author(s): Kaufman, Larry; Nesor, Harvey; Bernstein, Harold; Baron, Judson R.
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 115
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865728
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Stability Characterization of Refractory Materials under High Velocity Atmospheric Flight Conditions. Part IV. Volume II. Calculation of the General Surface Reaction Problem.
Report Number: AFML TR 69-84 Part 4 Volume 2
Author(s): Bernstein, Harold; Baron, Judson R.
Corporate Author: ManLabs Inc.
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 144
Contract: AF 33(615)-3859
Project: 7312
Task: 731201
AD Number: AD0865729
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On Thermal And Mechanical Effects At Sliding Interfaces
Report Number: AFML TR 69-91
Author(s): Ling, F. F.
Corporate Author:
Publication Date: 4/1/1969
Project: 0
Task: 0
AD Number: AD0693207
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Compatibility of Tankage Materials with Liquid Propellants
Report Number: AFML TR 69-99
Author(s): Tiffany, C. F.; Lorenz, P. M.
Corporate Author: Boeing Co Seattle WA Space Div
Publication Date: 5/1/1969
Project: 0
Task: 0
AD Number: AD0853957
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Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part I - The Phase Diagrams of the Systems Ti-Nb-C, Ti-Ta-C, and Ti-Mo-C
Report Number: AFML TR 69-117 Part 1
Author(s): E. Rudy
Corporate Author: Aerojet-General Corporation
Publication Date: 8/1/1970
Pages: 132
Project: 0
Task: 0
AD Number: AD0713153
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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
Report Number: AFML TR 69-117 Part 2
Author(s): C. E. Brukl
Corporate Author: Aerojet-General Corporation
Publication Date: 8/1/1969
Pages: 22
Project: 0
Task: 0
AD Number: AD0695063
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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
Report Number: AFML TR 69-117 Part 4
Author(s): C. E. Brukl
Corporate Author: Aerojet-General Corporation
Publication Date: 8/1/1969
Pages: 44
Project: 0
Task: 0
AD Number: AD0695062
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Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part V - The Phase Diagram W-B-C
Report Number: AFML TR 69-117 Part 5
Author(s): E. Rudy
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1970
Pages: 62
Contract: F33615-67-C-1513
Project: 7350
Task: 735001
AD Number: AD0713154
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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
Report Number: AFML TR 69-117 Part 6
Author(s): P. H. Booker and C. E. Brukl
Corporate Author: Aerojet-General Corporation
Publication Date: 12/1/1969
Pages: 73
Project: 0
Task: 0
AD Number: AD0700985
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Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part VII - The Phase Diagram Ti-V-C
Report Number: AFML TR 69-117 Part 7
Author(s): E. Rudy
Corporate Author: Aerojet-General Corporation
Publication Date: 8/1/1970
Pages: 64
Project: 0
Task: 0
AD Number: AD0713150
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Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part IX - Calculation of Thermodynamic Quantities from Phase Diagrams
Report Number: AFML TR 69-117 Part 9
Author(s): E. Rudy
Corporate Author: Aerojet-General Corporation
Publication Date: 8/1/1970
Pages: 42
Project: 0
Task: 0
AD Number: AD0713712
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Stress Waves in a Laminated Medium Generated by Transverse Forces
Report Number: AFML TR 69-120
Author(s): Voelker, Leonard E.; Achenbach, Jan D.
Corporate Author:
Publication Date: 8/1/1969
Project: 0
Task: 0
AD Number: AD0860372
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Analytical Approach to Composite Behavior
Report Number: AFML TR 69-129
Author(s): Ebert, L. J.; Fedor, R. J.; Hamilton, C. H.; Hecker, S. S.; Wright, P. K.
Corporate Author: Case Western Reserve Univ Cleveland OH Dept Of Metallurgy
Publication Date: 6/1/1969
Project: 0
Task: 0
AD Number: AD0857059
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Design Allowables for TITANIUM Alloys
Report Number: AFML TR 69-161
Author(s): Sommer, Alfred W.; Martin, Gardner R.
Corporate Author: North American Rockwell Corp Los Angeles CA Los Angeles Div
Publication Date: 6/1/1969
Project: 0
Task: 0
AD Number: AD0857807
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Torsion Testing of Aluminum at High Rates of Strain
Report Number: AFML TR 69-172
Author(s): Nicholas, Theodore; Garey, George F.
Corporate Author:
Publication Date: 7/1/1969
Project: 0
Task: 0
AD Number: AD0859808
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Plastic Flow And The Stress Concentration In Mild Steel Specimens
Report Number: AFML TR 69-193
Author(s): Bily, M.; Williams,T. R. G.
Corporate Author:
Publication Date: 7/1/1969
Project: 0
Task: 0
AD Number: AD0692489
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Microstructural Appearance Of The Discontinuity In Mild Steel
Report Number: AFML TR 69-194
Author(s): Bily, Matej; Williams, Thomas R. G.
Corporate Author: Southampton Univ (England) Inst Of Sound And Vibration Research
Publication Date: 7/1/1969
Project: 0
Task: 0
AD Number: AD0692490
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Manufacture of Superalloy Yarns
Report Number: AFML TR 69-205
Author(s): Gorton,Clair A.
Corporate Author:
Publication Date: 7/1/1969
Project: 0
Task: 0
AD Number: AD0859701
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Reinforced Thermoplastics For Making An Expandable, Rigidizable Wing Tip Tank
Report Number: AFML TR 69-212
Author(s): Salyer, I. O.; North, C. J.; Schwendeman, J. L.; Ohanian, Norick
Corporate Author: Monsanto Research Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 281
Features: + Foldout(s)
Contract: F33615-67-C-1542
Project: 7381
Task: 738101
AD Number: AD0699588
Photo Enhancement: Complete
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Evaluation of Commercially Available Eddy Current Equipment
Report Number: AFML TR 69-221
Author(s):
Corporate Author:
Publication Date: 5/1/1970
Project: 0
Task: 0
AD Number: AD0872681
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Manufacturing Methods for Aircraft Tires by Filament-Winding Techniques. Part I.
Report Number: AFML TR 69-226
Author(s): Sanger, Merle J.; Landes, Robert E.; Warner, Darrel M.; Waldo, Howard W.
Corporate Author: Aerojet-General Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1969
Pages: 431
Features: + Foldout(s)
Contract: F33615-67-C-1726
Project: 360-7
AD Number: AD0864955
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Investigation of Advanced Filament Wound Aircraft Landing Gear Structures
Report Number: AFML TR 69-229
Author(s): Yurenka, Steven
Corporate Author: McDonnell Douglas Corp Long Beach CA Douglas Aircraft Div
Laboratory: Air Force Materials Laboratory
Publication Date: 1/1/1970
Pages: 181
Features: + Foldout(s)
Contract: F33616-67-C-1717
Project: 7381
Task: 738101
AD Number: AD0871275
Photo Enhancement: Incomplete
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Relationship of Structure to Strength in Titanium Alloys
Report Number: AFML TR 69-236
Author(s): Breedis, John F.; Koul, M. Kishen
Corporate Author: Massachusetts Inst Of Tech Cambridge
Laboratory: Air Force Materials Laboratory
Publication Date: 6/1/1969
Pages: 63
Contract: AF33(615)-3866
Project: 7351
Task: None Given
AD Number: AD0861322
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Thermodynamics of Titanium Alloys. II. The Titanium-Aluminum System.
Report Number: AFML TR 69-248 Part 2
Author(s): Usell, R. J. Hoch, M.
Corporate Author: University of Cincinnati
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 24
Contract: AF33(615)-3865
Project: 7351
Task: 735103
AD Number: AD0865702
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Thermodynamics of Titanium Alloys. III. The Titanium-Molybdenum System.
Report Number: AFML TR 69-248 Part 3
Author(s): Hoch, M.; Viswanathan, R.
Corporate Author: University of Cincinnati
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 12
Contract: AF33(615)-3865
Project: 7351
Task: 735103
AD Number: AD0864931
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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.
Report Number: AFML TR 69-255
Author(s): Kaufman, J. G.; Schilling, P. E.; Nordmark, G. E.; Lifka, B. W.; Coursen, J. W.
Corporate Author: Aluminum Company of America
Laboratory: Air Force Materials Laboratory
Publication Date: 11/1/1969
Pages: 309
Contract: F33615-67-C-1521
Project: 7381
Task: 738106
AD Number: AD0864895
Photo Enhancement: Incomplete
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The Compatibilities of Boron and Germanium
Report Number: AFML TR 69-258
Author(s): Bidwell, Lawrence R.
Corporate Author: Air Force Materials Laboratory
Laboratory: Air Force Materials Laboratory
Publication Date: 10/1/1969
Pages: 29
Features: + Diagram(s) + Photo(s)
Contract: Laboratory Research - No Contract
Project: 7353
Task: None Given
AD Number: AD0863815
Photo Enhancement: Complete
Abstract Text:
The salient features of the boron-germanium phase equilibrium diagram were deduced from X-ray diffraction, metallographic, thermal analysis, and electron microprobe studies on both sintered and melted alloys. The system can be characterized as a classical monotecticeutectic with no intermediate phases. The occurrence of hypomonotectic boron crystals and boron crystals grown from a germanium melt indicates a slight solubility of germanium in solid boron and of boron in liquid germanium at the monotectic temperature. X-ray diffraction, thermal analysis, and metallographic studies indicate that the germanium-rich liquid freezes as essentially pure germanium and that the solid solubility of germanium in boron and of boron in germanium is virtually nil at the eutectic temperature. The minute quantity of boron that does dissolve in solid germanium does so substitutionally with a 0.01 to 0.02 volume percent contraction of the germanium lattice. These results indicate that germanium may have utility as a boron diffusion barrier for boron fiber-reinforced metal-matrix composites.
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Development of Carbide-Strengthened Niobium Alloys. Part I. Molybdenum in Niobium-Carbon Alloys.
Report Number: AFML TR 69-259 Part 1
Author(s): Ostermann, F.; Kibbey, E. E.
Corporate Author:
Laboratory: Air Force Materials Laboratory
Publication Date: 10/1/1969
Pages: 25
Contract: Laboratory Research - No Contract
Project: 7351
Task: 735106
AD Number: AD0863284
Photo Enhancement: Incomplete
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Tensile Properties of Beryllium at High Strain Rates and Temperatures
Report Number: AFML TR 69-273
Author(s): Schierloh, F. L.; Babcock, S. G.
Corporate Author: General Motors Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 10/1/1969
Pages: 55
Contract: F33615-69-C-1496
Project: 7351
Task: None Given
AD Number: AD0865380
Photo Enhancement: Incomplete
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Orientation of Small Diameter Discontinuous Reinforcements for Structural Composites
Report Number: AFML TR 69-288
Author(s):
Corporate Author: Owens-Corning Fiberglas Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 11/1/1969
Pages: 98
Contract: F33615-67-C-1736
Project: 7340
Task: None Given
AD Number: AD0867060
Photo Enhancement: Incomplete
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The Evaluation of the Mechanical Behavior of Metal Matrix Composites Reinforced with SiC-Coated, Boron Fibers. Volume II. Appendices.
Report Number: AFML TR 69-291 Volume 2
Author(s): Long, James R.
Corporate Author: Harvey Engineering Laboratories
Laboratory: Air Force Materials Laboratory
Publication Date: 11/1/1969
Pages: 157
Contract: F33615-67-C-1708
Project: 7351
Task: 735107
AD Number: AD0865014
Photo Enhancement: Incomplete
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Research on Deformation and Possible Strengthening Mechanisms for Solid Solution Phases of Titanium.
Report Number: AFML TR 69-293
Author(s): Cass, Thomas R.; Spencer, William R.
Corporate Author: Martin Marietta Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 66
Contract: AF33(615)-3863
Project: 7351
Task: None Given
AD Number: AD0864122
Photo Enhancement: Incomplete
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A Study of the Effectiveness of Selected Aniwear Additives in Synthetic Esters
Report Number: AFML TR 69-301
Author(s): Kenneth A. Davis, Major, USAF
Corporate Author: Air Force Materials Laboratory
Laboratory: Air Force Materials Laboratory
Publication Date: 7/1/1970
Pages: 76
Contract: Laboratory Research - No Contract
Project: 7343
Task: None Given
AD Number: AD0711667
Photo Enhancement: Not Needed
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Spatial Decay in the Response of Damped Periodic Structures, Part II.
Report Number: AFML TR 69-308 Part 2
Author(s): Y. K. Lin and R. Vaicaitis
Corporate Author: University of Illinois
Laboratory: Air Force Materials Laboratory
Publication Date: 8/1/1970
Pages: 23
Contract: F33615-67-C-1190
Project: 7351
Task: 735106
AD Number: AD0875857
Photo Enhancement: Not Needed
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Chemical Vapor Deposition (CVD) Barrel Coating for Refractory Fasteners
Report Number: AFML TR 69-316
Author(s): Wakefield, Gene F.; Yaws, Carl L.
Corporate Author: Texas Instruments, Incorporated
Laboratory: Air Force Materials Laboratory
Publication Date: 12/1/1969
Pages: 241
Contract: F33615-68-C-1433
Project: 474-8
Task: None Given
AD Number: AD0865504
Photo Enhancement: Incomplete
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Fatigue, Tensile and Creep Properties of 17-7 PH TH 1050 and AM 350 SCT Sheet
Report Number: AFML TR 69-331
Author(s): Bass, Colin D.; Harmsworth, C. L.
Corporate Author: Air Force Materials Lab Wright-Patterson AFB OH
Publication Date: 3/1/1970
Project: 0
Task: 0
AD Number: AD0871174
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An Improved Process for the Working of Welded Titanium Alloy Tubing
Report Number: AFML TR 69-333
Author(s): Huber, R. F.; Loewenstein, P.
Corporate Author: Whittaker Corporation
Laboratory: Air Force Materials Laboratory
Publication Date: 2/1/1970
Pages: 49
Contract: F33615-68-C-1364
Project: 116-8
Task: None Given
AD Number: AD0864987
Photo Enhancement: Incomplete
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