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Ternary Phase Equilibrium In Transition Metal-Boron-Carbon-Silicon Systems. Part II. Ternary Systems. Volume XII. Ti-Zr-B System. Investigation Of Pseudo-Binary Systems Zrb2-Nbb2, Zrb2-Tab2, And Hfb2-Nbn2
Author(s): Eckert, T. E.
Corporate Author(s): Aerojet-General Corp Sacramento CA Materials Research Lab
Laboratory: Air Force Materials Laboratory
Date of Publication: 1967-01
Report number: AFML TR 65-2 Part 2 Volume 12
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Mechanisms Associated With Long Time Creep Phenomena. Part II: Evaluation Of Long Time Creep Results.
Author(s): Widmer, R., Dhosi, J. M., Grant, N. J.
Corporate Author(s): New England Materials laboratory, Inc.
Laboratory: Air Force Materials Laboratory
Date of Publication: 1967-03
Report number: AFML TR 65-181 Part 2
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Storage Stability Of High Temperature Fuels
Author(s): Whisman, M. L., Ward, C. C.
Corporate Author(s): Bureau Of Mines Bartlesville Okla Petroleum Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1967-02
Report number: AFAPL TR 65-13 Part 3
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Ternary Phase Equilibria In Transition Metal-Boron-Carbon-Silicon Systems. Part II. Ternary Systems. Volume XVII. Constitution Of Ternary Ta-Mo-C Alloys
Author(s): Rudy, E., Windisch, St., Brukl, C. E.
Corporate Author(s): Aerojet-General Corp Sacramento Calif Materials Research Lab
Laboratory: Air Force Materials Laboratory
Date of Publication: 1967-12
Report number: AFML TR 65-2 Part 2 Volume 17
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SYSTRAN (Systems Analysis Translator): A Digital Computer Program. Supplement Two
Author(s): Weis, E. B., Lajeunesse, D. J.
Corporate Author(s): Research and Technology Division; Aerospace Medical Research Laboratories;
Laboratory: Aerospace Medical Research Laboratories
Date of Publication: 1967-12
Report number: AMRL TR 65-133 (Sup. II)
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The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part I. Description And Dynamic Tests Of An F-80 Model
Author(s): Statler, Irving C., Tufts, Orren B., Hirtreiter, Walter J.
Corporate Author(s): Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-02
Report number: AFFDL TR 66-153 Part 1
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The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part II. Dynamic Tests Of An F-104 Model.
Author(s): Statler, Irving C.
Corporate Author(s): Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-02
Report number: AFFDL TR 66-153 Part 2
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Low Pressure Type Expandable Aircraft Tire Characteristics
Author(s): Wagner, Paul M.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report number: AFFDL TR 66-170
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Application Of The Subdomain (Biezeno-Koch) Method To Circular Plate Bending
Author(s): Adams, O. E., Jr
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1967-06
Report number: AFFDL TR 66-215
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Measurement Of The Diffraction Correction Of The Gulton Model P420m-6 Microphone
Author(s): Ortega, Jose C.
Corporate Author(s): Western Electro-Acoustic Lab Inc Santa Monica CA
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1967-05
Report number: AFFDL TR 66-223

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