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Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 1. Summary of Mechanical and Physical Property Data Collected, Including Tensile Creep and Fatigue
Author(s): Hughes, P. J.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-01
Report number: ASD TDR 62-335 Volume 1
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Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 3. Tables of Data Collected
Author(s): None Given
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-01
Report number: ASD TDR 62-335 Volume 3
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Flight Test Investigation of Transonic Shock-Boundary Layer Phenomena
Author(s): Cahill, Jones F., Cooper, Bill L.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-07
Report number: AFFDL TR 68-84 Volume 1
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A Theoretical Investigation of a Circular Lifting Jet in a Cross-Flowing Mainstream
Author(s): Hackett, J. E., Miller, H. R.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1971-01
Report number: AFFDL TR 70-170
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Implementation Studies for a Reliability-Based Static Strength Criteria System: Volume I, Evaluation
Author(s): Campion, M. C., Morcock, D. S., Bateh, E. J., Huggins, W. J., Thompson, B. R., Muller, George E., Hanson, L. C.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-02
Report number: AFFDL TR 71-178 Volume 1
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Implementation Studies for a Reliability-Based Static Strength Criteria System: Volume II, Implementation
Author(s): Campion, M. C., Chapman, J. W., Bateh, E. J., Huggins, W. J., Thompson, B. R., Muller, George E., Campbell, W. D.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-02
Report number: AFFDL TR 71-178 Volume 2
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Response of Aircraft to Three Dimensional Random Turbulence
Author(s): Eichenbaum, Frederick D.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-10
Report number: AFFDL TR 72-28
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Evaluation of the Flying Qualities Requirements of MIL-F-8785B(ASG) Using the C-5A Airplane
Author(s): Silvers, Charles L., Withers, Clifton C.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-03-20
Report number: AFFDL TR 75-3
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Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 2a. Details Of Data Collection Program. Test Techniques And Results For Tension, Compression, Bearing, Shear, Crippling, Joints, And Physical Properties
Author(s): McGee, W. M., Matthews, B. R.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-12
Report number: ASD TDR 62-335 Volume 2A
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Determination Of Design Data For Heat Treated Titanium Alloy Sheet. Volume 2b. Test Techniques And Results For Creep And Fatigue
Author(s): White, D. L., Watson, H. T.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-12
Report number: ASD TDR 62-335 Volume 2B

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